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searching for Wing loading 465 found (3227 total)

Schleicher ASW 15 (768 words) [view diff] exact match in snippet view article find links to article

63 km/h (39 mph, 34 kn) at wing loading of 28.9 kg/m2 (5.9 lb/sq ft) Never exceed speed: 220 km/h (140 mph, 120 kn) at wing loading of 28.9 kg/m2 (5.9 lb/sq ft)

Canard (aeronautics) (4,253 words) [view diff] exact match in snippet view article

aircraft designer may adopt the canard configuration to reduce the main wing loading, to better control the main wing airflow, or to increase the aircraft's

Parachute (8,438 words) [view diff] exact match in snippet view article find links to article

this wing loading. Professional canopy pilots compete with wing loading of 10 to over 15 kilograms per square meter. While ram-air parachutes with wing loading

Kawasaki Ki-60 (1,376 words) [view diff] exact match in snippet view article find links to article

the wing loading was 181.76 kg/m2 (37.23 lb/ft2), which was extremely high by Japanese standards (the standard IJAAF fighter, the Ki-27, had a wing loading

Howard DGA-8 (722 words) [view diff] exact match in snippet view article find links to article

exceeded airline leg room with limousine-like spaciousness. With its high wing loading, the Howards rode through most turbulence with airline-like solidity

Schempp-Hirth Janus (633 words) [view diff] exact match in snippet view article find links to article

5 lb/sq ft) wing loading Rate of sink: 0.6 m/s (120 ft/min) at 90 km/h (49 kn; 56 mph) at 36.5 kg/m2 (7.5 lb/sq ft) wing loading Wing loading: 40 kg/m2

Dwarf dog-faced bat (1,965 words) [view diff] exact match in snippet view article find links to article

free-tailed bat, with exceptionally broad wingtips. Additionally, it has low wing loading, meaning that it has a large wing surface area relative to its body weight

Wingtip vortices (2,651 words) [view diff] exact match in snippet view article find links to article

Depending on ambient atmospheric humidity as well as the geometry and wing loading of aircraft, water may condense or freeze in the core of the vortices

NAL/ADE Pushpak (204 words) [view diff] exact match in snippet view article find links to article

features Cleaner Aerodynamics, Nose-mounted payload, high endurance and low wing loading. The Pushpak is powered by electric motor and has a flight endurance

Convair YB-60 (985 words) [view diff] exact match in snippet view article find links to article

000 mi (13,000 km, 7,000 nmi) Service ceiling: 53,300 ft (16,200 m) Wing loading: 57.3 lb/sq ft (280 kg/m2) Armament Guns: 2 × 20 mm (0.787 in) cannon

SZD-17X Jaskółka L (767 words) [view diff] exact match in snippet view article find links to article

ratio: 31.2 Rate of sink: 0.8 m/s (160 ft/min) at 87 km/h (47 kn; 54 mph) Wing loading: 39.7 kg/m2 (8.1 lb/sq ft) Note: A. Glass quotes different specifications:

Slingsby Prefect (943 words) [view diff] exact match in snippet view article find links to article

It was about 20 kg heavier than its predecessor, but despite a higher wing loading had a significantly better lift to drag ratio, 21 compared with 17. The

Kawasaki Ki-28 (537 words) [view diff] no match in snippet view article find links to article

the Nakajima Ki-27 was by far the most maneuverable and had the lowest wing-loading. On this basis, the Ki-27 was selected by the Imperial Japanese Army

Yakovlev Yak-15 (2,146 words) [view diff] exact match in snippet view article find links to article

retract into the fuselage. Low and high wing loading wing versions were considered, but the low wing loading 15-square-meter (160 sq ft) wings were chosen

Sikorsky S-18 (218 words) [view diff] exact match in snippet view article find links to article

side-valve, water-cooled, piston engine, 150 hp (110 kW) each Performance Wing loading: 7.4 lb/sq ft (36.2 kg/m2) max load "The Russian Years". www.sikorskyarchives

Horten H.I (736 words) [view diff] exact match in snippet view article find links to article

10 kg/m2 (2.0 lb/sq ft) wing loading Lift-to-drag: 21:1 at 72 km/h (45 mph; 39 kn) and 10 kg/m2 (2.0 lb/sq ft) wing loading Wing loading: 10 kg/m2 (2.0 lb/sq ft)

Miles M.26 (677 words) [view diff] exact match in snippet view article find links to article

11 was to be eight-engined, with high cruising speed (for 1943), high wing loading and low power loading, seating at least 50 passengers, but was rejected

Schleicher ASG 32 (604 words) [view diff] exact match in snippet view article find links to article

(170 mph, 150 kn) Maximum glide ratio: 52 Wing loading: 54.1 kg/m2 (11.1 lb/sq ft) (max.) Min. wing loading: 33.8 kg/m2 (6.9 lb/sq ft) with one 70 kg

Sikorsky S-17 (173 words) [view diff] exact match in snippet view article find links to article

water-cooled, piston engine, 150 hp (110 kW) Propellers: 2-bladed Performance Wing loading: 5.6 lb/sq ft (27.4 kg/m2) max load "S-17". ram-home.com. 4 September

Sikorsky S-12 (291 words) [view diff] exact match in snippet view article find links to article

Propellers: 2-bladed Performance Service ceiling: 12,070 ft (3,680 m) Wing loading: 7.1 lb/sq ft (34.5 kg/m2) max load Finne, K.N. (1987). Igor Sikorsky:

Aerola Alatus (464 words) [view diff] exact match in snippet view article find links to article

skids. The bubble canopy is in one piece and is removable. The light wing loading and low stall speed mean that the aircraft can be flown in the smallest

Schreder HP-20 (330 words) [view diff] exact match in snippet view article find links to article

versus 113 sq ft (10.5 m2) for the HP-19. This gives the HP-20 a higher wing loading and higher best glide speed, although the glide ratio is the same as

Swinny's horseshoe bat (844 words) [view diff] exact match in snippet view article find links to article

surface area of their wings is comparatively larger resulting in decreased wing loading. This leads to limited dispersal and restricted range between populations

CubCrafters CC11-160 Carbon Cub SS (676 words) [view diff] exact match in snippet view article find links to article

airspeed indicator, achievable in powered flight pitched for dive with 1G wing loading in smooth air. Range: 390 nmi (450 mi, 720 km) maximum, using 24.0 gal

Schempp-Hirth Standard Austria (709 words) [view diff] exact match in snippet view article find links to article

class aircraft. The design aims were to produce an aircraft with a low wing loading and a high lift/drag ratio, which necessitated low weight and low drag

Douglas C-1 (661 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 14,850 ft (4,530 m) Rate of climb: 645 ft/min (3.28 m/s) Wing loading: 8 lb/sq ft (39 kg/m2) Power/mass: 0.0676 hp/lb (0.1111 kW/kg) Notes

Vought FU (446 words) [view diff] exact match in snippet view article find links to article

Range: 357 nmi (410 mi, 660 km) Service ceiling: 26,500 ft (8,080 m) Wing loading: 10.3 lb/sq ft (50.2 kg/m2) Power/mass: 0.079 hp/lb (0.13 kW/kg) Climb

Schempp-Hirth Discus (765 words) [view diff] no match in snippet view article find links to article

wing mounted ballast tanks are in use (184 L combined) for a maximum wing-loading of 50 kg/m2 (10 lb/sq ft) The Discus dominated standard class sailplane

Martin XLB-4 (225 words) [view diff] exact match in snippet view article find links to article

525 hp (391 kW) each Performance Maximum speed: 69 mph (111 km/h, 60 kn) Wing loading: 9.98 lb/sq ft (48.7 kg/m2) Related development Huff-Daland XHB-1 Aircraft

Douglas O-43 (483 words) [view diff] exact match in snippet view article find links to article

800 m) Time to altitude: 5,000 ft (1,500 m) in 3 minutes 18 seconds Wing loading: 15.8 lb/sq ft (77 kg/m2) Power/mass: 0.127 hp/lb (0.209 kW/kg) Armament

Lockheed XB-30 (538 words) [view diff] exact match in snippet view article find links to article

5,333 mi (8,045 km, 4,634 nmi) Service ceiling: 17,832 ft (5,440 m) Wing loading: 52 lb/sq ft (255 kg/m2) Power/mass: 0.10 hp/lb (170 W/kg) Armament Guns:

Sikorsky S-9 (287 words) [view diff] exact match in snippet view article find links to article

Propellers: 2-bladed Performance Maximum speed: 56 mph (90 km/h, 49 kn) Wing loading: 6.8 lb/sq ft (33 kg/m2) max load Sikorsky, Igor (1944). The Story of

Tupolev ANT-1 (371 words) [view diff] exact match in snippet view article find links to article

73 kn) Range: 540 km (335 mi, 291 nmi) Service ceiling: 400 m (1,300 ft) Wing loading: 36 kg/m2 (7.4 lb/sq ft) Andrei Tupolev Tupolev Wikimedia Commons has

Kawanishi K6K (249 words) [view diff] exact match in snippet view article find links to article

Endurance: 6 hours Time to altitude: 3,000 m (9,800 ft) in 11 minutes Wing loading: 60 kg/m2 (12 lb/sq ft) Power/mass: 5.3 kg/kW (8.7 lb/hp) Mikesh, Robert

Allstar SZD-54 Perkoz (2,134 words) [view diff] exact match in snippet view article find links to article

as a safety cockpit according to the 2016 CS-22 standard. The maximum wing loading of the aerobatic version is 36.1 kg/m2, of the 20-metre version is 35

Vought XF3U (380 words) [view diff] exact match in snippet view article find links to article

Range: 570 mi (917 km, 500 nmi) Service ceiling: 25,300 ft (7,700 m) Wing loading: 18 lb/sq ft (88 kg/m2) Power/mass: 0.13 hp/lb (0.22 kW/kg) Armament

Slingsby Grasshopper (351 words) [view diff] exact match in snippet view article find links to article

30 mph (48 km/h, 26 kn) Never exceed speed: 80 mph (129 km/h, 70 kn) Wing loading: 3.10 lb/sq ft (15.13 kg/m2) Air Training Corps Aircraft of comparable

Schreder Airmate HP-8 (632 words) [view diff] exact match in snippet view article find links to article

wing is of only 110 square feet (10 m2) in area and this gives a high wing loading of 7.53 lbs/sq ft (36.8 kg/m2), allowing a high glide ratio at a high

Fish locomotion (5,929 words) [view diff] exact match in snippet view article find links to article

higher wing loading and lift to drag ratios for flying fish compared to a comparably sized bird. Differences in wing area, wing span, wing loading, and

Sikorsky S-11 (329 words) [view diff] exact match in snippet view article find links to article

speed: 63 mph (102 km/h, 55 kn) Stall speed: 43 mph (70 km/h, 38 kn) Wing loading: 7.9 lb/sq ft (38.6 kg/m2) max load Sikorsky, Igor (1944). The Story

Tupolev I-12 (242 words) [view diff] exact match in snippet view article find links to article

pusher propellers Performance Maximum speed: 300 km/h (190 mph, 160 kn) Wing loading: 80 kg/m2 (16 lb/sq ft) Power/mass: 0.326 kW/kg (0.198 hp/lb) Armament

Stearman XA-21 (471 words) [view diff] exact match in snippet view article find links to article

223 kn (257 mph, 414 km/h) Cruise speed: 174 kn (200 mph, 322 km/h) Wing loading: 30.0 lb/sq ft (147 kg/m2) Power/mass: 0.15 hp/b (250 W/kg) Armament

Schreder Airmate HP-10 (536 words) [view diff] exact match in snippet view article find links to article

(35.5 mph) 229 km (142 miles) goal and return flight. With its high wing loading of 6.75 lb/sq ft (33.0 kg/m2) and small wing area of 114 sq ft (10.6

SZD-27 (360 words) [view diff] exact match in snippet view article find links to article

8 m/s (160 ft/min) at 80 km/h (50 mph; 43 kn) Lift-to-drag: +8 / -4 g Wing loading: 28.6 kg/m2 (5.9 lb/sq ft) Aircraft of comparable role, configuration

Keystone B-5 (401 words) [view diff] exact match in snippet view article find links to article

Range: 815 mi (1,310 km, 707 nmi) Service ceiling: 14,000 ft (4,270 m) Wing loading: 273.3 lb/sq ft (52.22 kg/m2) Power/mass: 0.0810 hp/lb (133 W/kg) Armament

Douglas XB-31 (575 words) [view diff] exact match in snippet view article find links to article

5,370 mi (8,640 km, 4,670 nmi) Service ceiling: 31,600 ft (9,600 m) Wing loading: 41 lb/sq ft (200 kg/m2) Power/mass: 0.066 hp/lb (0.109 kW/kg), later

Bell X-16 (523 words) [view diff] exact match in snippet view article find links to article

2,867 nmi (3,319 mi, 5,310 km) Service ceiling: 71,832 ft (21,900 m) Wing loading: 33 lb/sq ft (160 kg/m2) Thrust/weight: 0.55 Aircraft of comparable role

Glidersport LightHawk (220 words) [view diff] exact match in snippet view article find links to article

wing employs a large wing area of 12 m2 (130 sq ft) to produce a low wing loading to allow the aircraft to make use of small and light sources of lift

Heinkel HD 30 (202 words) [view diff] exact match in snippet view article find links to article

Range: 700 km (430 mi, 380 nmi) Service ceiling: 4,650 m (15,260 ft) Wing loading: 47 kg/m2 (9.6 lb/sq ft) de Agostini. World Aviation. Heinkel: HD 25

Tupolev I-8 (382 words) [view diff] exact match in snippet view article find links to article

000 m (3,300 ft) in 1 minute 5,000 m (16,000 ft) in 6 minutes 42 seconds Wing loading: 71 kg/m2 (15 lb/sq ft) Power/mass: 0.327 kW/kg (0.199 hp/lb) Armament

SZD-48 Jantar Standard 2/3 (1,150 words) [view diff] exact match in snippet view article find links to article

without ballast Minimum sink speed: 97 km/h (52 kn; 60 mph) with ballast Wing loading: 50.7 kg/m2 (10.4 lb/sq ft) Data from Jane's All the World's Aircraft

Midwest MU-1 (428 words) [view diff] exact match in snippet view article find links to article

36 mph (58 km/h) Rate of sink: 174 ft/min (0.88 m/s) at 30 mph (48 km/h) Wing loading: 3 lb/sq ft (15 kg/m2) Related lists List of gliders Said, Bob: 1983

SZD-11 Albatros (340 words) [view diff] exact match in snippet view article find links to article

Niespał. With wings of greater span, and reduced empty weight, the wing loading was reduced, markedly improving the climb performance over the 16m-span

Keystone B-4 (499 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 14,000 ft (4,300 m) Rate of climb: 580 ft/min (30 m/s) Wing loading: 11.31 lb/sq ft (55.22 kg/m2) Power/mass: 0.0888 hp/lb (146 W/kg) Armament

Canadian Vickers Varuna (316 words) [view diff] exact match in snippet view article find links to article

14,000 ft (4,300 m) Time to altitude: 5,000 ft (1,500 m) in 9 minutes Wing loading: 7.4 lb/sq ft (36 kg/m2) Power/mass: 0.0377 hp/lb (0.0620 kW/kg) Grey

Eclipse Project (322 words) [view diff] exact match in snippet view article find links to article

examine the feasibility of towing a delta wing aircraft having high wing loading, validate the tow simulation model, and demonstrate various operational

Arado W 2 (254 words) [view diff] exact match in snippet view article find links to article

1 m/s (200 ft/min) Time to altitude: 2,000 m (6,600 ft) in 35 minutes Wing loading: 37 kg/m2 (7.6 lb/sq ft) Power/mass: 0.0812 kW/kg (0.0494 hp/lb) Grey

Canadian Vickers Varuna (316 words) [view diff] exact match in snippet view article find links to article

14,000 ft (4,300 m) Time to altitude: 5,000 ft (1,500 m) in 9 minutes Wing loading: 7.4 lb/sq ft (36 kg/m2) Power/mass: 0.0377 hp/lb (0.0620 kW/kg) Grey

OMRE OE-01 (970 words) [view diff] exact match in snippet view article find links to article

The wing design evolved into a high aspect ratio of 23:1, a modest wing loading of 20 kg/m2 and light alloy stressed skin structure, giving a smooth

Hawker P.1072 (659 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 44,500 ft (13,600 m) Rate of climb: 5,000 ft/min (25 m/s) Wing loading: 53 lb/sq ft (260 kg/m2) Thrust/weight: 0.51 UK portal Aviation portal

Dassault Mirage 2000 (12,585 words) [view diff] exact match in snippet view article find links to article

particular design, thereby reducing the wing loading. The wing on a Mirage 2000 has an area of 41 m2, giving it a wing loading of some 77 lb/sq ft at a takeoff

Schleicher Ka 2 Rhönschwalbe (909 words) [view diff] exact match in snippet view article find links to article

Ka-2 was found to be lower than expected, due to the relatively high wing loading. Schleicher introduced the Ka2b, increasing the wingspan from 15 m (49 ft)

Aero A.17 (108 words) [view diff] exact match in snippet view article find links to article

Empty weight: 47 kg (104 lb) Gross weight: 127 kg (280 lb) Performance Wing loading: 7.4 kg/m2 (1.5 lb/sq ft) Related lists List of gliders "J2mcL Planeurs

AEG B.II (253 words) [view diff] exact match in snippet view article find links to article

Range: 1,130 km (700 mi, 610 nmi) Service ceiling: 3,000 m (9,800 ft) Wing loading: 27 kg/m2 (5.5 lb/sq ft) Related development AEG C.I Wilberg, Thomas

Boeing Model 853-21 Quiet Bird (262 words) [view diff] exact match in snippet view article find links to article

ceiling: 47,000 ft (14,000 m) Rate of climb: 3,050 ft/min (15.5 m/s) Wing loading: 45.4 lb/sq ft (221 kg/m2) Thrust/weight: 0.52 Related development Boeing

Douglas O-31 (763 words) [view diff] exact match in snippet view article find links to article

(7.70 m/s) Time to altitude: 10,000 ft (3,000 m)7 minutes 12 seconds Wing loading: 14.6 lb/sq ft (71 kg/m2) Power/mass: 0.12 hp/lb (0.20 kW/kg) Armament

Harlow PJC-2 (686 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 15,500 ft (4,700 m) Rate of climb: 800 ft/min (4.1 m/s) Wing loading: 14.05 lb/sq ft (68.6 kg/m2) Power/mass: 0.056 hp/lb (0.092 kW/kg) Aircraft

Avia 51 (1,295 words) [view diff] exact match in snippet view article find links to article

painting, and lacquering. The aircraft possessed a relatively high wing loading (19.3 lb./sq.ft.) and thus also had a somewhat high landing speed; a

Martin Baltimore (2,178 words) [view diff] exact match in snippet view article find links to article

were during takeoffs and landings due to the aircraft's fairly high wing loading, high approach speed and a directional stability problems during takeoffs

Sikorsky Cypher (511 words) [view diff] exact match in snippet view article find links to article

depending on model Endurance: 2-3 hours Service ceiling: 8,000 ft (2,440 m) Wing loading: 9.9 lb/sq ft (47.5 kg/m2) Power/mass: 0.2 hp/lb (0.32 kW/kg) Avionics

Tupolev Tu-125 (301 words) [view diff] exact match in snippet view article find links to article

7,000 km (4,300 mi, 3,800 nmi) Service ceiling: 25,000 m (82,000 ft) Wing loading: 487 kg/m2 (100 lb/sq ft) Thrust/weight: 0.4076 Armament Missiles: 1

Hamburger Flugzeugbau HFB 209 (345 words) [view diff] exact match in snippet view article find links to article

from the engines, rated at 3,500 ehp for takeoff, together with the low wing loading and large, low-pressure tyres, gave good short- and rough-field performance

Curtiss-Reid Rambler (773 words) [view diff] exact match in snippet view article find links to article

000 ft (4,300 m) Absolute ceiling Rate of climb: 750 ft/min (3.8 m/s) Wing loading: 6.075 lb/sq ft (29.66 kg/m2) Power/mass: 16.5 lb/hp (10.0 kg/kW) Molson

Nieuport 17 (4,682 words) [view diff] exact match in snippet view article find links to article

larger engine of the latter aircraft made it nose heavy and increased the wing loading, especially when armed with a synchronised Vickers gun. Developed in

Seversky XP-41 (316 words) [view diff] exact match in snippet view article find links to article

Range: 730 mi (1,168 km, 630 nmi) Service ceiling: 31,500 ft (9,600 m) Wing loading: 30.1 lb/sq ft (147.1 kg/m2) Power/mass: 0.18 hp/lb (0.30 kW/kg) Armament

Rolladen-Schneider LS1 (1,084 words) [view diff] exact match in snippet view article find links to article

ballasts of 2 x 90 liters instead of 2 x 45 liters, increasing the maximal wing loading from 40 to 45 kg/m2 (hence the name) (2 built). Data from General characteristics

Tupolev Tu-80 (662 words) [view diff] exact match in snippet view article find links to article

(5,104 mi, 4,435 nmi) estimated Service ceiling: 11,180 m (36,680 ft) Wing loading: 363 kg/m2 (74 lb/sq ft) Power/mass: 0.13 kW/kg (0.079 hp/lb) Armament

Aero A.46 (148 words) [view diff] exact match in snippet view article find links to article

ceiling: 4,850 m (15,910 ft) Rate of climb: 2.783 m/s (547.8 ft/min) Wing loading: 46 kg/m2 (9.4 lb/sq ft) Power/mass: 0.150 W/kg (0.09 hp/lb) "Aero A-46 :

Tupolev I-4 (406 words) [view diff] exact match in snippet view article find links to article

Range: 524 km (326 mi, 283 nmi) Service ceiling: 7,655 m (25,115 ft) Wing loading: 60 kg/m2 (12 lb/sq ft) Power/mass: 0.25 kW/kg (0.15 hp/lb) Armament

Douglas T2D (628 words) [view diff] exact match in snippet view article find links to article

(landplane) 5,000 ft (1,500 m) in 7 minutes 42 seconds (floatplane) Wing loading: 11.4 lb/sq ft (56 kg/m2) (landplane) 11.9 lb/sq ft (58 kg/m2) (floatplane)

Kawasaki Ki-78 (483 words) [view diff] exact match in snippet view article find links to article

Range: 600 km (370 mi, 320 nmi) Service ceiling: 8,000 m (26,000 ft) Wing loading: 209 kg/m2 (43 lb/sq ft) Power/mass: 0.373 kW/kg (0.2273 hp/lb) Aircraft

Mitsubishi A7M (1,513 words) [view diff] exact match in snippet view article find links to article

MK9 promised more horsepower. With the larger, more powerful engine, wing loading became an issue. The Navy requested at most 150 kg/m2, but wanted 130 kg/m2

AEG B.I (186 words) [view diff] exact match in snippet view article find links to article

speed: 100 km/h (62 mph, 54 kn) Service ceiling: 2,500 m (8,200 ft) Wing loading: 24 kg/m2 (4.9 lb/sq ft) Aircraft of comparable role, configuration,

Delta Sailplane Nomad (413 words) [view diff] exact match in snippet view article find links to article

with a 36.1 ft (11.0 m) span wing, wing area of 147 sq ft (13.7 m2), wing loading of 2.77 lb/sq ft (13.5 kg/m2) and a cruise speed of 55 mph (89 km/h)

Boeing Model 6D (472 words) [view diff] exact match in snippet view article find links to article

000 ft (3,700 m) Time to altitude: 3,400 ft (1,000 m) in 10 minutes Wing loading: 7.4 lb/sq ft (36 kg/m2) Power/mass: 0.09 hp/lb (0.15 kW/kg) Wikimedia

Farman HF.7 (152 words) [view diff] exact match in snippet view article find links to article

pusher propeller Performance Maximum speed: 90 km/h (56 mph, 49 kn) Wing loading: 20.0 kg/m2 (4.1 lb/sq ft) Power/mass: 0.08 hp/kg Hartmann, Gérard. Les

Pfalz D.VIII (397 words) [view diff] exact match in snippet view article find links to article

hour 30 minutes Time to altitude: 6,000 m (20,000 ft) in 25 minutes Wing loading: 42.9 kg/m2 (8.8 lb/sq ft) Power/mass: 0.16 kW/kg (0.097 hp/lb) Armament

Boeing XB-39 Superfortress (590 words) [view diff] exact match in snippet view article find links to article

290 mi (10,060 km, 5,460 nmi) Service ceiling: 35,000 ft (11,000 m) Wing loading: 69.12 lb/sq ft (337.5 kg/m2) Power/mass: 0.073 hp/lb (121 W/kg) Armament

Jonker JS-1 Revelation (679 words) [view diff] exact match in snippet view article find links to article

performance gives a claimed best glide of around 1:60 and, with the maximum wing loading of 58.7 kg/m2 and the polar remaining flat at high cruise speeds, the

Tupolev Tu-75 (686 words) [view diff] exact match in snippet view article find links to article

4,140 km (2,570 mi, 2,240 nmi) Service ceiling: 9,500 m (31,200 ft) Wing loading: 338.9 kg/m2 (69.4 lb/sq ft) Power/mass: 0.1395 kW/kg (0.0849 hp/lb)

Nihon L7P (425 words) [view diff] exact match in snippet view article find links to article

200 ft/min) Time to altitude: 3,000 m (9,800 ft) in 6 minutes 51 seconds Wing loading: 117.7 kg/m2 (24.1 lb/sq ft) Power/mass: 6.5 kg/kW (10.7 lb/hp) "Nihon

Arado V I (331 words) [view diff] exact match in snippet view article find links to article

2,000 km (1,200 mi, 1,100 nmi) Service ceiling: 4,000 m (13,000 ft) Wing loading: 50 kg/m2 (10 lb/sq ft) Power/mass: 0.1596 kW/kg (0.0971 hp/lb) "Arado

Lockheed Explorer (453 words) [view diff] exact match in snippet view article find links to article

5,500 mi (8,850 km, 4,800 nmi) Rate of climb: 1,200 ft/min (6.1 m/s) Wing loading: 28.8 lb/sq ft (140.5 kg/m2) Related development Lockheed Vega Lockheed

Caudron C.91 (437 words) [view diff] exact match in snippet view article find links to article

166 km/h (103 mph, 90 kn) Time to altitude: 56 min t 4,000 m (13,123 ft) Wing loading: 38.6 kg/m2 (7.9 lb/sq ft) Hauet, André (2001). Les Avions Caudrons.

Northrop C-19 Alpha (552 words) [view diff] exact match in snippet view article find links to article

at sea level 550 ft/min (168 m/min) Seaplane at 10,000 ft (3,048 m) Wing loading: 15.25 lb/sq ft (74.5 kg/m2) 15.9 lb/sq ft (78 kg/m2) Seaplane Power/mass:

Tupolev Tu-1 (623 words) [view diff] exact match in snippet view article find links to article

2,250 km (1,400 mi, 1,210 nmi) Service ceiling: 11,000 m (36,000 ft) Wing loading: 261.37 kg/m2 (53.53 lb/sq ft) Armament Guns: 2 × 45 mm Nudelman-Suranov

Piaggio P.119 (1,145 words) [view diff] exact match in snippet view article find links to article

(43 ft) wingspan. The surface area was almost 28 m2 (300 ft2), giving a wing loading of around 150 kg/m2. The wing was built on a single spar which also supported

SIAI-Marchetti SM.101 (309 words) [view diff] exact match in snippet view article find links to article

Range: 1,250 km (780 mi, 670 nmi) Service ceiling: 4,800 m (15,700 ft) Wing loading: 73.2 kg/m2 (15.0 lb/sq ft) Power/mass: 12.71 kg/kW (20.9 lb/hp) Related

Colomban MC-30 Luciole (804 words) [view diff] exact match in snippet view article find links to article

full approval from the LAA. LAA approval was required as the Luciole's wing loading of 43.5 kg/m2 was too high to benefit from original UK SSDR microlight

Tupolev ANT-16 (540 words) [view diff] exact match in snippet view article find links to article

(3,300 ft) in 12 minutes 24 seconds 2,000 m (6,600 ft) in 34 minutes Wing loading: 79 kg/m2 (16 lb/sq ft) Power/mass: 0.101 kW/kg (0.061 hp/lb) Take-off

Sikorsky S-10 (448 words) [view diff] exact match in snippet view article find links to article

270 nmi) Time to altitude: 500 m (1,600 ft) in 5 minutes 20 seconds Wing loading: 22 kg/m2 (4.5 lb/sq ft) Power/mass: 0.06 kW/kg (0.036 hp/lb) Sikorsky

Potez XIX (334 words) [view diff] exact match in snippet view article find links to article

540 ft) Time to altitude: 2,000 m (6,600 ft) in 9 minutes 33 seconds Wing loading: 42.5 kg/m2 (8.7 lb/sq ft) Power/mass: 0.0864 hp/lb (0.1420 kW/kg) Armament

Ryan XF2R Dark Shark (492 words) [view diff] exact match in snippet view article find links to article

ceiling: 39,100 ft (11,900 m) Rate of climb: 4,850 ft/min (24.6 m/s) Wing loading: 36.1 lb/sq ft (176 kg/m2) Armament Guns: 4 × .50-inch (12.7 mm) M2 Browning

Tupolev Tu-116 (623 words) [view diff] exact match in snippet view article find links to article

10,750 km (6,680 mi, 5,800 nmi) Service ceiling: 12,000 m (39,000 ft) Wing loading: 421 kg/m2 (86 lb/sq ft) Power/mass: 0.168 kW/kg (0.102 hp/lb) Wikimedia

Sukhoi Su-17 (1949) (394 words) [view diff] exact match in snippet view article

altitude: 4 minutes to 10,000 m (33,000 ft) (Research variant 3.5 minutes) Wing loading: 287 kg/m2 (59 lb/sq ft) Armament 2 x 37 mm (1.457 in) Nudelman N-37

Arado Ar 69 (325 words) [view diff] exact match in snippet view article find links to article

400 ft) Time to altitude: 1,000 m (3,280 ft) in 3 minutes 24 seconds Wing loading: 32.85 kg/m2 (6.73 lb/sq ft) Power/mass: 4.54 kg/hp "Arado Ar 69". Wehrmacht-History

Douglas XP3D (790 words) [view diff] exact match in snippet view article find links to article

(5,800 m) Time to altitude: 5,000 ft (1,500 m) in 6 minutes 6 seconds Wing loading: 17.7 lb/sq ft (86 kg/m2) Power/mass: 0.0565 hp/lb (0.0929 kW/kg) Armament

Breda A.3 (323 words) [view diff] exact match in snippet view article find links to article

75 km/h (47 mph, 40 kn) Endurance: 6h Service ceiling: 4,000 m (13,000 ft) Wing loading: 38 kg/m2 (7.8 lb/sq ft) Armament Guns: 3x 7.7 mm (0.30 in) Lewis guns

Heinkel HD 16 (269 words) [view diff] exact match in snippet view article find links to article

speed: 196 km/h (122 mph, 106 kn) Service ceiling: 4,000 m (13,000 ft) Wing loading: 47 kg/m2 (9.6 lb/sq ft) Wikimedia Commons has media related to Heinkel

Darling's horseshoe bat (309 words) [view diff] exact match in snippet view article find links to article

while its belly is pale gray. It has a low aspect ratio and very low wing loading, meaning that its flight speed is likely slow but highly maneuverable

Macchi M.53 (449 words) [view diff] exact match in snippet view article find links to article

Endurance: 4 hours Time to altitude: 1,000 m (3,300 ft) in 12 minutes Wing loading: 42.7 kg/m2 (8.7 lb/sq ft) Power/mass: 0.0875 kW/kg (0.0532 hp/lb) Italian

Ilyushin I-21 (467 words) [view diff] exact match in snippet view article find links to article

000 ft/min) Time to altitude: 5,000 metres (16,000 ft) in 3.8 to 4.6 minutes Wing loading: 116 kg/m2 (24 lb/sq ft) Power/mass: 0.59 hp/kg Take-off run: 190 m (620 ft)

Aero A.21 (229 words) [view diff] exact match in snippet view article find links to article

500 m (21,300 ft) Time to altitude: 21 min 3 s to 3,000 m (9,800 ft) Wing loading: 36 kg/m2 (7.4 lb/sq ft) Czechoslovakia. Related development Aero A.11

Heinkel HE 9 (256 words) [view diff] exact match in snippet view article find links to article

300 ft) in 2 minutes 50 seconds: 5,000 m (16,000 ft) in 25 minutes' Wing loading: 63 kg/m2 (13 lb/sq ft) Wikimedia Commons has media related to Heinkel

Yakovlev Yak-26 (410 words) [view diff] exact match in snippet view article find links to article

2,200 km (1,400 mi, 1,200 nmi) Service ceiling: 16,000 m (52,000 ft) Wing loading: 386 kg/m2 (79 lb/sq ft) Thrust/weight: 0.36 Armament 4 x 23 mm Nudelman

Keystone B-3 (770 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 12,700 ft (3,870 m) Rate of climb: 530 ft/min (2.7 m/s) Wing loading: 11.31 lb/sq ft (55.42 kg/m2) Power/mass: 0.0811 hp/lb (133 W/kg) Armament

Bréguet 11 Corsaire (320 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 6,000 m (20,000 ft) Rate of climb: 4.86 m/s (957 ft/min) Wing loading: 32 kg/m2 (6.6 lb/sq ft) (at max. takeoff weight) Power/mass: 0.15 kW/kg

Leonard Annebula (438 words) [view diff] exact match in snippet view article find links to article

Cherokee II's 23:1 glide ratio to 31.5:1. The Annebula also has more span, wing loading and a higher aspect ratio than the Cherokee II. The fuselage was also

Arado S I (308 words) [view diff] exact match in snippet view article find links to article

(3,300 ft) in 10 minutes; 2,000 m (6,600 ft) in 22 minutes 30 seconds Wing loading: 30 kg/m2 (6.1 lb/sq ft) Power/mass: 0.0861 kW/kg (0.0524 hp/lb) Wikimedia

Yakovlev Yak-50 (1949) (504 words) [view diff] exact match in snippet view article

ceiling: 16,050 m (52,660 ft) Rate of climb: 68 m/s (13,400 ft/min) Wing loading: 260 kg/m2 (53 lb/sq ft) Thrust/weight: 0.65 Armament Guns: 2× 23 mm

Farman HF.6 (180 words) [view diff] exact match in snippet view article find links to article

Maximum speed: 90 km/h (56 mph, 49 kn) Range: 315 km (196 mi, 170 nmi) Wing loading: 26.1 kg/m2 (5.3 lb/sq ft) Power/mass: 0.09 hp/kg "Farman HF.14". Premiers

Albatros Dr.II (235 words) [view diff] exact match in snippet view article find links to article

145 kW (194 hp) Propellers: 2-bladed fixed-pitch propeller Performance Wing loading: 25.4 kg/m2 (5.2 lb/sq ft) Power/mass: 0.16 kW/kg (0.097 hp/lb) Gray

Polikarpov ITP (699 words) [view diff] exact match in snippet view article find links to article

(37,700 ft) Time to altitude: six minutes to 5,000 metres (16,000 ft) Wing loading: 216 kg/m2 (44 lb/sq ft) Armament Guns: 3 × 20 mm ShVAK cannons, 200

Breda-Zappata BZ.309 (296 words) [view diff] exact match in snippet view article find links to article

500–3,000 m (8,200–9,800 ft) Service ceiling: 7,000 m (23,000 ft) + Wing loading: 161 kg/m2 (33 lb/sq ft) at 5,950 kg (13,120 lb) "Italians Start Work

Keystone B-6 (765 words) [view diff] exact match in snippet view article find links to article

Range: 825 mi (1,330 km, 717 nmi) Service ceiling: 14,100 ft (6,400 m) Wing loading: 11.66 lb/sq ft (56.92 kg/m2) Power/mass: 0.0861 hp/lb (142 W/kg) Armament

Slingsby Kirby Cadet (283 words) [view diff] exact match in snippet view article find links to article

weight: 297 lb (134.5 kg) Gross weight: 513 lb (232.7 kg) Performance Wing loading: 3.0 lb/sq ft (14.7 kg/m2) Related development Slingsby Kirby Tutor Slingsby

PZL-112 Junior (346 words) [view diff] exact match in snippet view article find links to article

(13,000 ft) g limits: +4.4/-1.8 Rate of climb: 3.50 m/s (689 ft/min) Wing loading: 65.56 kg/m2 (13.43 lb/sq ft) Related development PZL-110 Koliber Wikimedia

Sikorsky S-20 (297 words) [view diff] exact match in snippet view article find links to article

400 ft) Time to altitude: 2,000 m (6,600 ft) in 6 minutes 20 seconds Wing loading: 33.0 kg/m2 (6.8 lb/sq ft) Power/mass: 0.21 hp/kg Armament Guns: 1 x

Wright Model D (400 words) [view diff] exact match in snippet view article find links to article

58.1 kn (66.9 mph, 107.7 km/h) Rate of climb: 525 ft/min (2.67 m/s) Wing loading: 5.83 lb/sq ft (28.5 kg/m2) Wikimedia Commons has media related to Wright

Kawanishi E13K (421 words) [view diff] exact match in snippet view article find links to article

950 ft) Time to altitude: 4,000 m (13,000 ft) in 9 minutes 14 seconds Wing loading: 104.4 kg/m2 (21.4 lb/sq ft) Power/mass: 5.2 kg/kW (8.6 lb/hp) Armament

Dart Aircraft (823 words) [view diff] exact match in snippet view article find links to article

31 ft. 9 in., 21 ft. and 130 sq. ft. At an all-up weight of 682 lb., the wing loading is 5.25 Ib./sq.ft. The Kitten II (G-AEXT) was also first flown in 1937

SZD-20X Wampir II (569 words) [view diff] exact match in snippet view article find links to article

44 kn) Rate of sink: 0.84 m/s (165 ft/min) at 72 km/h (45 mph; 39 kn) Wing loading: 17.8 kg/m2 (3.6 lb/sq ft) Aircraft of comparable role, configuration

CANT 26 (343 words) [view diff] exact match in snippet view article find links to article

Range: 810 km (500 mi, 440 nmi) Service ceiling: 3,800 m (12,500 ft) Wing loading: 25 kg/m2 (5.1 lb/sq ft) Power/mass: 0.238 kW/kg (0.145 hp/lb) Grey,

Glaser-Dirks DG-600 (512 words) [view diff] exact match in snippet view article find links to article

+5.8 -3.8 Maximum glide ratio: 46 Rate of sink: 0.56 m/s (110 ft/min) Wing loading: 47.94 kg/m2 (9.82 lb/sq ft) max NOTE: The following data represent later

General Dynamics X-62 VISTA (837 words) [view diff] exact match in snippet view article find links to article

ceiling: 50,000 ft (15,000 m) + Rate of climb: 50,000 ft/min (250 m/s) Wing loading: 88.2 lb/sq ft (431 kg/m2) Thrust/weight: 1.095 Related development General

Wright Micron (424 words) [view diff] exact match in snippet view article find links to article

designed and built the Wright MPA Mk 1, which first flew in 1972. The low wing loading of that design affected the flight opportunities which could be made

Waco CG-13 (632 words) [view diff] exact match in snippet view article find links to article

195 mph (314 km/h, 169 kn) 150 mph (130 kn; 241 km/h) with flaps down Wing loading: 21.65 lb/sq ft (105.7 kg/m2) Related development Waco CG-4 Waco CG-15

Westland Walrus (568 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 19,000 ft (5,800 m) Rate of climb: 950 ft/min (4.8 m/s) Wing loading: 10.8 lb/sq ft (53 kg/m2) Power/mass: 0.09 hp/lb (0.15 kW/kg) Armament

Aeromot AMT-200 Super Ximango (409 words) [view diff] exact match in snippet view article find links to article

Rate of climb: 1.8 m/s (350 ft/min) Rate of sink: .93 m/s (183 ft/min) Wing loading: 45.3 kg/m2 (9.3 lb/sq ft) Taylor 1996, p. 511. Taylor, Michael JH (1996)

Breda A.8 (296 words) [view diff] exact match in snippet view article find links to article

(109 mph, 94 kn) Endurance: 6h Service ceiling: 3,500 m (11,500 ft) Wing loading: 39 kg/m2 (8.0 lb/sq ft) Armament Guns: 3x 7.7 mm (0.30 in) Lewis machine-guns

Grigorovich M-23bis (302 words) [view diff] exact match in snippet view article find links to article

propeller Performance Maximum speed: 165 km/h (103 mph, 89 kn) estimated Wing loading: 35 kg/m2 (7.2 lb/sq ft) Shavrov, V.B. (1994). Istoriia konstruktskii

Heinkel HD 19 (426 words) [view diff] exact match in snippet view article find links to article

116 kn) Cruise speed: 182 km/h (113 mph, 98 kn) Service ceiling: 6,400 m (21,000 ft) Wing loading: 47 kg/m2 (9.6 lb/sq ft) "Heinkel HD-19". www.airwar.ru.

Lockheed XF-90 (1,186 words) [view diff] exact match in snippet view article find links to article

ceiling: 39,000 ft (11,890 m) Rate of climb: 5,555 ft/min (28.2 m/s) Wing loading: 79 lb/sq ft (386 kg/m2) Thrust/weight: 0.30 Armament 6 × 20 mm (.79

IIL IS-11 (620 words) [view diff] exact match in snippet view article find links to article

Rate of sink: 0.82 m/s (161 ft/min) minimum, at 68 km/h (42 mph; 37 kn) Wing loading: 23.8 kg/m2 (4.9 lb/sq ft) Taylor, John W. R. (1981). Jane's All the

Caudron C.161 (283 words) [view diff] exact match in snippet view article find links to article

engine, 52 kW (70 hp) Performance Maximum speed: 150 km/h (93 mph, 81 kn) Wing loading: 28.6 kg/m2 (5.9 lb/sq ft) Power/mass: 0.0912 kW/kg (0.0555 hp/lb) Wikimedia

Aero A.38 (246 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 4,800 m (15,700 ft) Rate of climb: 1.77 m/s (348 ft/min) Wing loading: 47 kg/m2 (9.6 lb/sq ft) Power/mass: 0.10 kW/kg (0.06 hp/lb) Wikimedia

Strojnik S-2 (571 words) [view diff] exact match in snippet view article find links to article

2-bladed folding Performance Stall speed: 38 mph (61 km/h, 33 kn) at a wing loading of 6.6 lb/sq ft Never exceed speed: 149 mph (240 km/h, 129 kn) Maximum

Piper PA-14 Family Cruiser (468 words) [view diff] exact match in snippet view article find links to article

Range: 499 mi (803 km, 434 nmi) Rate of climb: 575 ft/min (2.92 m/s) Wing loading: 10.32 lb/sq ft (50.4 kg/m2) Power/mass: 0.062 hp/lb (0.102 kW/kg) Piper

Fokker F-10 (788 words) [view diff] exact match in snippet view article find links to article

420 ft/min (7.2 m/s) Time to altitude: 10,000 ft (3,000 m) in 10 minutes Wing loading: 15.8 lb/sq ft (77 kg/m2) Power/mass: 9.05 lb/hp (5.50 kg/kW) Related

Scheibe SF-33 (157 words) [view diff] exact match in snippet view article find links to article

(450 ft/min) Rate of sink: 0.8 m/s (160 ft/min) at 70 km/h (38 kn; 43 mph) Wing loading: 32.99 kg/m2 (6.76 lb/sq ft) "Scheibe SF-33". Taylor, Michael J. H. (1989)

Huff-Daland XB-1 (447 words) [view diff] exact match in snippet view article find links to article

Range: 700 mi (1,100 km, 610 nmi) Service ceiling: 15,000 ft (4,600 m) Wing loading: 5.899 lb/sq ft (28.80 kg/m2) Power/mass: 0.072 hp/lb (120 W/kg) Armament

Göppingen Gö 1 (490 words) [view diff] exact match in snippet view article find links to article

of sink: 0.96 m/s (189 ft/min) Lift-to-drag: 17 at 72 km/h (45 mph) Wing loading: 14.66 kg/m2 (3.00 lb/sq ft) Aircraft of comparable role, configuration

Heinkel He 57 (246 words) [view diff] exact match in snippet view article find links to article

ceiling: 3,800 m (12,500 ft) Time to altitude: 5 min to 1,000 m (3,300 ft) Wing loading: 62.3 kg/m2 (12.75 lb/sq ft) Landing speed: 93 km/h (58 mph; 50 kn) Wikimedia

Civil Aviation Department Revathi (443 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 3,505 m (11,499 ft) Rate of climb: 3 m/s (590 ft/min) Wing loading: 68.2 kg/m2 (14.0 lb/sq ft) Power/mass: 0.112 kW/kg (0.068 hp/lb) Taylor

Sikorsky S-16 (463 words) [view diff] exact match in snippet view article find links to article

08 m/s (400 ft/min) Time to altitude: 1,000 m (3,300 ft) in 8 minutes Wing loading: 26.8 kg/m2 (5.5 lb/sq ft) Power/mass: 0.14 hp/kg Armament Guns: 1 x

Aero A.29 (242 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 6,700 m (22,000 ft) Rate of climb: 1.74 m/s (343 ft/min) Wing loading: 46 kg/m2 (9.4 lb/sq ft) Power/mass: 0.110 kW/kg (0.07 hp/lb) Armament

ICA IS-32 (325 words) [view diff] exact match in snippet view article find links to article

sink: 0.62 m/s (122 ft/min) *Minimum sink speed: 90 km/h (49 kn; 56 mph) Wing loading: 40.2 kg/m2 (8.2 lb/sq ft) John W.R. Taylor, ed. (1988). Jane's All the

Macchi M.70 (680 words) [view diff] exact match in snippet view article find links to article

altitude: 7 mins to 1,000 m (3,281 ft) 53 mins to 4,000 m (13,123 ft) Wing loading: 26 kg/m2 (5.3 lb/sq ft) Power/mass: 0.0764 kg/kw (0.0476 lbs/hp) Alenia

Lockheed XC-35 (930 words) [view diff] exact match in snippet view article find links to article

ceiling: 31,500 ft (9,600 m) Rate of climb: 1,125 ft/min (5.72 m/s) Wing loading: 22.9 lb/sq ft (112 kg/m2) Power/mass: 0.105 hp/lb (0.173 kW/kg) Related

Aero A.26 (209 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 6,000 m (20,000 ft) Rate of climb: 2.25 m/s (443 ft/min) Wing loading: 31 kg/m2 (6.3 lb/sq ft) Power/mass: 0.120 kW/kg (0.073 hp/lb) Armament

Blohm & Voss P 212 (462 words) [view diff] exact match in snippet view article find links to article

521 kn) at 7,000 metres (23,000 ft) Rate of climb: 21.3 m/s (4,190 ft/min) Wing loading: 310 kg/m2 (63 lb/sq ft) Armament Aircraft of comparable role, configuration

Curtiss-Reid Courier (1,004 words) [view diff] exact match in snippet view article find links to article

000 ft (4,600 m) Rate of climb: 820 ft/min (4.2 m/s) with full load Wing loading: 12.1 lb/sq ft (59 kg/m2) Molson, K.M.; Taylor, H.A. (1982). Canadian

Savoia-Marchetti SM.93 (596 words) [view diff] exact match in snippet view article find links to article

000 m (32,800 ft) Time to altitude: 4,000 m (13,000 ft) in 5 min 10 sec Wing loading: 176.9 kg/m2 (36.2 lb/sq ft) Power/mass: 0.2 kW/kg (0.122 hp/lb) Armament

Avro Avocet (387 words) [view diff] exact match in snippet view article find links to article

speed: 133 mph (214 km/h, 116 kn) Service ceiling: 23,000 ft (7,000 m) Wing loading: 8.1 lb/sq ft (40 kg/m2) Power/mass: 0.092 hp/lb (0.151 kW/kg) Armament

Douglas O-38 (1,018 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 19,000 ft (5,800 m) Rate of climb: 1,500 ft/min (7.6 m/s) Wing loading: 12 lb/sq ft (59 kg/m2) Power/mass: 0.12 hp/lb (0.20 kW/kg) Armament

Grigorovich MR-2 (300 words) [view diff] exact match in snippet view article find links to article

200 m (13,800 ft) Time to altitude: 1,000 m (3,281 ft) in 7.0 minutes Wing loading: 49.0 kg/m2 (10.0 lb/sq ft) Armament Guns: 1-2 x machine guns Shavrov

SZD-8 Jaskółka (652 words) [view diff] exact match in snippet view article find links to article

51 mph) Rate of sink: 0.75 m/s (148 ft/min) at 75 km/h (40 kn; 47 mph) Wing loading: 7.34 kg/m2 (1.50 lb/sq ft) Aircraft of comparable role, configuration

Avro 641 Commodore (405 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 11,500 ft (3,500 m) Rate of climb: 700 ft/min (3.6 m/s) Wing loading: 11.4 lb/sq ft (56 kg/m2) Power/mass: 0.061 hp/lb (0.100 kW/kg) Related

Blériot-SPAD S.51 (564 words) [view diff] exact match in snippet view article find links to article

2 m/s (1,420 ft/min) Time to altitude: 4,000 m (13,000 ft) in 9 minutes Wing loading: 52.6 kg/m2 (10.8 lb/sq ft) Power/mass: 0.24537 kW/kg (0.14925 hp/lb)

SZD-22 Mucha Standard (820 words) [view diff] exact match in snippet view article find links to article

40 kn) Rate of sink: 0.73 m/s (144 ft/min) at 71 km/h (44 mph; 38 kn) Wing loading: 27.4 kg/m2 (5.6 lb/sq ft) (SZD-22A), 30 kg/m2 (6.144 lb/sqft) – (SZD-22B

Bloch MB.110 (135 words) [view diff] exact match in snippet view article find links to article

speed: 210 km/h (130 mph, 110 kn) Service ceiling: 7,300 m (24,000 ft) Wing loading: 61 kg/m2 (12 lb/sq ft) "Bloch MB-110 - avion de police coloniale - Un

Breda A.9 (301 words) [view diff] exact match in snippet view article find links to article

(500 mi, 430 nmi) Endurance: 3 hours Service ceiling: 6,000 m (20,000 ft) Wing loading: 39 kg/m2 (8.0 lb/sq ft) Power/mass: 0.196 kW/kg (0.119 hp/lb) Related

Sukhoi Su-11 (733 words) [view diff] exact match in snippet view article find links to article

ceiling: 18,000 m (59,000 ft) Rate of climb: 136.7 m/s (26,910 ft/min) Wing loading: 76.09 kg/m2 (15.58 lb/sq ft) [citation needed] Thrust/weight: 0.71 Take-off

Heston JC.6 (436 words) [view diff] exact match in snippet view article find links to article

speed: 125 mph (201 km/h, 109 kn) Range: 745 mi (1,199 km, 647 nmi) Wing loading: 11.3 lb/sq ft (55 kg/m2) Aircraft of comparable role, configuration

Tupolev Tu-85 (976 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 11,700 m (38,400 ft) Rate of climb: 17 m/s (3,300 ft/min) Wing loading: 277 kg/m2 (57 lb/sq ft) Power/mass: 0.170 kW/kg (0.103 hp/lb)[citation

SZD-51 Junior (501 words) [view diff] exact match in snippet view article find links to article

80 km/h (50 mph) Rate of sink: 0.59 m/s (116 ft/min) at 72 km/h (45 mph) Wing loading: 28.4 kg/m2 (5.8 lb/sq ft) Aircraft of comparable role, configuration

PZL-102 Kos (508 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 3,800 m (12,500 ft) Rate of climb: 3.5 m/s (690 ft/min) Wing loading: 57.2 kg/m2 (11.7 lb/sq ft) Power/mass: 0.1126 kW/kg (0.0685 hp/lb) Taylor

IIL IS-8 (726 words) [view diff] exact match in snippet view article find links to article

Rate of sink: 0.98 m/s (193 ft/min) minimum, at 70 km/h (43 mph; 38 kn) Wing loading: 25.8 kg/m2 (5.3 lb/sq ft) Taylor, John W. R. (1981). Jane's All the

IIL IS-10 (689 words) [view diff] exact match in snippet view article find links to article

Rate of sink: 0.67 m/s (132 ft/min) minimum, at 72 km/h (45 mph; 39 kn) Wing loading: 25.7 kg/m2 (5.3 lb/sq ft) Taylor, John W. R. (1981). Jane's All the

Boeing YQM-94 B-Gull (1,021 words) [view diff] exact match in snippet view article find links to article

period. Boeing choose the Cessna 172 because its approach speed and wing loading were close to that of the YQM-94. At the end of 1971, the YQM-94 remote

Nieuport 16 (2,138 words) [view diff] exact match in snippet view article find links to article

configuration made the aircraft dangerously nose-heavy and increased the wing loading which compromised manoeuvrability. The British would continue with the

Sikorsky S-41 (864 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 18,210 ft (5,550 m) Rate of climb: 875 ft/min (4.45 m/s) Wing loading: 18.93 lb/sq ft (92.4 kg/m2) Power/mass: 12 lb/hp (7.3 kg/kW) Related

SZD-51 Junior (501 words) [view diff] exact match in snippet view article find links to article

80 km/h (50 mph) Rate of sink: 0.59 m/s (116 ft/min) at 72 km/h (45 mph) Wing loading: 28.4 kg/m2 (5.8 lb/sq ft) Aircraft of comparable role, configuration

Polikarpov TB-2 (267 words) [view diff] exact match in snippet view article find links to article

800 m (22,300 ft) Time to altitude: 3,000 m (9,800 ft) in 12 minutes Wing loading: 53 kg/m2 (11 lb/sq ft) Power/mass: 0.110 kW/kg (0.067 hp/lb) Take-off

Focke-Wulf S 2 (233 words) [view diff] exact match in snippet view article find links to article

500 m (11,500 ft) Time to altitude: 1,000 m (3,300 ft) in 9 minutes Wing loading: 37.2 kg/m2 (7.6 lb/sq ft) Power/mass: 0.074 kW/kg (0.045 hp/lb) Grey

Nakajima C3N (441 words) [view diff] exact match in snippet view article find links to article

2,278 km (1,415 mi, 1,230 nmi) Service ceiling: 6,670 m (21,880 ft) Wing loading: 100 kg/m2 (20 lb/sq ft) Power/mass: 0.2081 kW/kg (0.1266 hp/lb) Armament

Yakovlev Yak-11 (1,195 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 7,100 m (23,295 ft) Rate of climb: 8.1 m/s (1,600 ft/min) Wing loading: 161 kg/m2 (32.9 lb/sq ft) Power/mass: 0.17 kW/kg (0.10 hp/lb) Armament

Schleicher ASK 23 (465 words) [view diff] exact match in snippet view article find links to article

50 mph) Rate of sink: 0.62 m/s (122 ft/min) at 74 km/h (40 kn; 46 mph) Wing loading: 29.5 kg/m2 (6.0 lb/sq ft) ::::ASK23B: 27.9 kg/m2 (5.7 lb/sq ft) Aircraft

Douglas 1211-J (455 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 50,000 ft (15,000 m) Rate of climb: 500 ft/min (2.5 m/s) Wing loading: 50 lb/sq ft (240 kg/m2) Armament Guns: 2x 20 mm (0.787 in) cannon Bombs:

Blackburn Blackburd (478 words) [view diff] exact match in snippet view article find links to article

400 m) Time to altitude: 6,500 ft (1,981 m) in 16 minutes 15 seconds Wing loading: 8.33 lb/sq ft (40.7 kg/m2) Power/mass: 0.061 hp/lb (0.100 kW/kg) Armament

Aero A.8 (203 words) [view diff] exact match in snippet view article find links to article

Cruise speed: 105 km/h (65 mph, 57 kn) Range: 600 km (370 mi, 320 nmi) Wing loading: 36.5 kg/m2 (7.5 lb/sq ft) "Aero, továrna letadel dr.Kabeš, Praha - Vysočany"

Letov Š-4 (330 words) [view diff] exact match in snippet view article find links to article

200 m (20,300 ft) Time to altitude: 3,000 m (9,800 ft) in 9.3 minutes Wing loading: 61.5 kg/m2 (12.6 lb/sq ft) Power/mass: 0.16 kW/kg (0.1 hp/lb) Armament

Waco CG-15 (442 words) [view diff] exact match in snippet view article find links to article

180 mph (290 km/h, 160 kn) 100 mph (87 kn; 161 km/h) with flaps lowered Wing loading: 12.9 lb/sq ft (63 kg/m2) [citation needed] Related development Waco

Lockheed Altair (809 words) [view diff] exact match in snippet view article find links to article

Range: 580 mi (935 km, 504 nmi) Service ceiling: 23,800 ft (7,255 m) Wing loading: 52.5 lb/sq ft (81.5 kg/m2) Power/mass: 0.10 hp/lb (0.17 kW/kg) Climb

Martin XB-68 (688 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 44,800 ft (13,650 m) Rate of climb: 500 ft/min (25 m/s) Wing loading: 85 lb/sq ft (414 kg/m2) Thrust/weight: 0.74 Armament Guns: 1× 20 mm

Slingsby Capstan (403 words) [view diff] exact match in snippet view article find links to article

41 kn) Rate of sink: 130 ft/min (0.66 m/s) at 43 mph (70 km/h; 38 kn) Wing loading: 5.7 lb/sq ft (27.7 kg/m2) List of gliders "Slingsby Archived 3 February

Sikorsky S-35 (924 words) [view diff] exact match in snippet view article find links to article

(233 km/h, 126 kn) Endurance: 7 hours Service ceiling: 16,800 ft (5,100 m) Wing loading: 21.8 lb/sq ft (106 kg/m2) Power/mass: 19 lb/hp Aircraft of comparable

Hamburger Flugzeugbau Ha 136 (360 words) [view diff] exact match in snippet view article find links to article

4 in) Wingspan: 6.6 m (21 ft 8 in) Height: 2.3 m (7 ft 7 in) Performance Wing loading: 70 kg/m2 (14 lb/sq ft) Pohlmann (1982) Amtmann (1998). Hans Amtmann;

Bell XP-83 (936 words) [view diff] exact match in snippet view article find links to article

7 m/s) Time to altitude: 30,000 ft (9,100 m) in 11 minutes 30 seconds Wing loading: 56 lb/sq ft (270 kg/m2) Thrust/weight: 0.33 Armament Guns: 6 × .50 in

Consolidated Vultee XP-81 (1,007 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 47,000 ft (14,000 m) Rate of climb: 5,300 ft/min (27 m/s) Wing loading: 106 lb/sq ft (520 kg/m2) Armament Guns: 6 × 20 mm (0.787 in) cannon

Grigorovich ROM-1 (411 words) [view diff] exact match in snippet view article find links to article

380 ft) Time to altitude: 1,000 m (3,281 ft) in 10 minutes 6 seconds Wing loading: 56.0 kg/m2 (11.5 lb/sq ft) Armament Guns: 4 x 7.62 mm (0.300 in) DA

Nakajima E2N (445 words) [view diff] exact match in snippet view article find links to article

hours Time to altitude: 3,000 m (9,800 ft) in 31 minutes 37 seconds Wing loading: 44.3 kg/m2 (9.1 lb/sq ft) Power/mass: 0.12 kW/kg (0.07 hp/lb) Armament

Comp Air 12 (153 words) [view diff] exact match in snippet view article find links to article

917 mi, 4,695 km) Rate of climb: 2,800 ft/min (14 m/s) at gross weight Wing loading: 35 lb/sq ft (170 kg/m2) Avionics Sebastian Communication / OP Technologies

Vultee XP-54 (937 words) [view diff] exact match in snippet view article find links to article

ceiling: 37,000 ft (11,300 m) Rate of climb: 2,300 ft/min (11.7 m/s) Wing loading: 40 lb/sq ft (196 kg/m2) Power/mass: 0.13 hp/lb (0.20 kW/kg) Armament

Letov Š-8 (197 words) [view diff] exact match in snippet view article find links to article

Range: 400 km (250 mi, 220 nmi) Service ceiling: 7,000 m (23,000 ft) Wing loading: 74.8 kg/m2 (15.3 lb/sq ft) Power/mass: 0.2834 kW/kg (0.1724 hp/lb) Aircraft

Bell XP-77 (1,083 words) [view diff] exact match in snippet view article find links to article

ceiling: 30,100 ft (9,180 m) Rate of climb: 3,600 ft/min (18.3 m/s) Wing loading: 40.28 lb/sq ft (196.5 kg/m2) Power/mass: .13 hp/lb (213 W/kg) Armament

Sikorsky S-37 (863 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 16,000 ft (4,900 m) Rate of climb: 600 ft/min (3.0 m/s) Wing loading: 13–15 lb/sq ft (63–73 kg/m2) max load Related development Sikorsky S-35

Sukhoi Su-10 (810 words) [view diff] exact match in snippet view article find links to article

(2,400 ft/min) Time to altitude: 10,000 m (33,000 ft) in 20 minutes Wing loading: 297 kg/m2 (61 lb/sq ft) Thrust/weight: 0.29 Take-off run: 1,000 m (3

Schleicher Poppenhausen (634 words) [view diff] exact match in snippet view article find links to article

glide ratio: best, 16.4 Rate of sink: 0.88 m/s (173 ft/min) minimum Wing loading: 13.5 kg/m2 (2.8 lb/sq ft) Wikimedia Commons has media related to Poppenhausen

PZL M-17 (482 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 6,500 m (21,300 ft) Rate of climb: 7.9 m/s (1,560 ft/min) Wing loading: 76.6 kg/m2 (15.7 lb/sq ft) Power/mass: 0.149 kW/kg (0.091 hp/lb) EM-11

PZL Bielsko SZD-55 (565 words) [view diff] exact match in snippet view article find links to article

(94–134 ft/min) *Minimum sink speed: 75–100 km/h (40–54 kn; 47–62 mph) Wing loading: 28.5–52.1 kg/m2 (5.8–10.7 lb/sq ft) Related lists List of gliders Wikimedia

SIAI-Marchetti SM.1019 (721 words) [view diff] exact match in snippet view article find links to article

ceiling: 7,620 m (25,000 ft) Rate of climb: 9.1833 m/s (1,807.74 ft/min) Wing loading: 80.4 kg/m2 (16.5 lb/sq ft) at 1,300 kg (2,900 lb) AUW; 89.7 kg/m2 (18

Junkers EF 126 (519 words) [view diff] exact match in snippet view article find links to article

189 nmi) 60% power Endurance: 45 min Rate of climb: 8.0 m/s (1,575 ft/min) Wing loading: 314 kg/m2 (32.6 lb/sq ft) Endurance: 23 mins (100% speed) Armament Guns:

Aero A.25 (241 words) [view diff] exact match in snippet view article find links to article

[citation needed] Rate of climb: 4 m/s (790 ft/min) [citation needed] Wing loading: 35 kg/m2 (7.2 lb/sq ft) [citation needed] Power/mass: 0.110 kW/kg (0

Lockheed XFV (1,015 words) [view diff] exact match in snippet view article find links to article

ceiling: 43,300 ft (13,100 m) Rate of climb: 10,820 ft/min (55.0 m/s) Wing loading: 65.9 lb/sq ft (322 kg/m2) Armament 4 × 20 mm (.79 in) cannons or 48

Weller ULI NG (457 words) [view diff] exact match in snippet view article find links to article

span wing has an area of 12.78 m2 (137.6 sq ft), giving a very light wing loading of 17.0 kg/m2 (3.5 lb/sq ft). The standard engine available is the 30 hp

Gulfstream G200 (794 words) [view diff] exact match in snippet view article find links to article

some of the field performance lost as a result of the Galaxy's higher wing loading. It used rubber de-ice boots on wing and horizontal stabilizer leading

Caudron C.60 (507 words) [view diff] exact match in snippet view article find links to article

000 m (13,000 ft) Time to altitude: 4,000 m (13,000 ft) in 36 minutes Wing loading: 33 kg/m2 (6.8 lb/sq ft) Power/mass: 0.1129 kW/kg (0.0687 hp/lb) Aviation

Lavochkin-Gorbunov-Gudkov LaGG-3 (4,001 words) [view diff] exact match in snippet view article find links to article

1st Series was heavier than the prototype which negatively affected wing loading, rate of climb, ceiling, and maneuverability. As a result, the LaGG-3

Tupolev Tu-70 (844 words) [view diff] exact match in snippet view article find links to article

2,500 km (1,600 mi, 1,300 nmi) Service ceiling: 11,000 m (36,000 ft) Wing loading: 361 kg/m2 (74 lb/sq ft) Power/mass: 0.14 kW/kg (0.085 hp/lb) Related

Aero A.18 (418 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 9,000 m (30,000 ft) Rate of climb: 9.8 m/s (1,930 ft/min) Wing loading: 55.8 kg/m2 (11.4 lb/sq ft) Power/mass: 0.1565 kW/kg (0.0952 hp/lb) Armament

Beriev Be-2500 (508 words) [view diff] exact match in snippet view article find links to article

(33,000 ft) Range in ground effect: 10,700 km (6,600 mi; 5,800 nmi) Wing loading: 730 kg/m2 (150 lb/sq ft) Thrust/weight: 0.00025 kN/kg (0.025 lbf/lb)

Stout Skycar (859 words) [view diff] exact match in snippet view article find links to article

Stall speed: 35 mph (56 km/h, 30 kn) Range: 320 mi (510 km, 280 nmi) Wing loading: 7.6 lb/sq ft (37 kg/m2) Power/mass: 19 lb/hp (12 kg/kW) Eckland, K.O

Hindustan Ardhra (270 words) [view diff] exact match in snippet view article find links to article

3 -2.65 Maximum glide ratio: 26 Rate of sink: 0.78 m/s (154 ft/min) Wing loading: 17.32 kg/m2 (3.55 lb/sq ft) "Ardra, Ārdrā, Ārdra: 32 definitions". 27

Nakajima E8N (792 words) [view diff] exact match in snippet view article find links to article

850 ft) Time to altitude: 3,000 m (9,800 ft) in 6 minutes 31 seconds Wing loading: 71.7 kg/m2 (14.7 lb/sq ft) Power/mass: 0.2491 kW/kg (0.1515 hp/lb) Armament

Caudron C.362 (638 words) [view diff] exact match in snippet view article find links to article

pitch propeller Performance Maximum speed: 350 km/h (220 mph, 190 kn) Wing loading: 100 kg/m2 (20 lb/sq ft) Wikimedia Commons has media related to Caudron

Peel Z-1 Glider Boat (482 words) [view diff] exact match in snippet view article find links to article

combined with the light gross weight of 600 lb (270 kg) give a very light wing loading of just 2.2 lb/sq ft (11 kg/m2). The lower wing tips feature wingtip

Grigorovich ROM-2 (370 words) [view diff] exact match in snippet view article find links to article

500 m (14,800 ft) Time to altitude: 1,000 m (3,281 ft) in 7.0 minutes Wing loading: 61.0 kg/m2 (12.5 lb/sq ft) Armament Guns: 4 × machine guns Шавров, В

Akaflieg Berlin B12 (1,072 words) [view diff] exact match in snippet view article find links to article

strenuous, requiring several ground-handlers high weight causes high wing loading, reducing thermalling performance (i.e. rate of climb). Once the quirks

Hindustan Ardhra (270 words) [view diff] exact match in snippet view article find links to article

3 -2.65 Maximum glide ratio: 26 Rate of sink: 0.78 m/s (154 ft/min) Wing loading: 17.32 kg/m2 (3.55 lb/sq ft) "Ardra, Ārdrā, Ārdra: 32 definitions". 27

Ader Éole (508 words) [view diff] exact match in snippet view article find links to article

15 kW (20 hp) Performance Maximum speed: 58 km/h (36 mph, 31 kn)164 ft Wing loading: 8 kg/m2 (1.6 lb/sq ft) Power/mass: 0.05 kW/kg (0.03 hp/lb) Alexander

SZD-18 Czajka (569 words) [view diff] exact match in snippet view article find links to article

31 kn) Rate of sink: 1.13 m/s (222 ft/min) at 51 km/h (32 mph; 28 kn) Wing loading: 14.4 kg/m2 (2.9 lb/sq ft) Aircraft of comparable role, configuration

Boeing C-32 (3,815 words) [view diff] exact match in snippet view article find links to article

650 nmi (6,500 mi, 10,460 km) Service ceiling: 42,000 ft (13,000 m) Wing loading: 127.88 lb/sq ft (624.4 kg/m2) Thrust/weight: 0.314 Take-off field length:

Schweizer SGU 1-2 (384 words) [view diff] exact match in snippet view article find links to article

Gross weight: 455 lb (206 kg) Performance Lift-to-drag: 10 (estimated) Wing loading: 2.31 lb/sq ft (11.3 kg/m2) Related lists List of gliders Schweizer,

Nakajima E8N (792 words) [view diff] exact match in snippet view article find links to article

850 ft) Time to altitude: 3,000 m (9,800 ft) in 6 minutes 31 seconds Wing loading: 71.7 kg/m2 (14.7 lb/sq ft) Power/mass: 0.2491 kW/kg (0.1515 hp/lb) Armament

Schleicher K 10 (532 words) [view diff] exact match in snippet view article find links to article

weight: 220 kg (485 lb) equipped Max takeoff weight: 320 kg (705 lb) Wing loading: 25.5 kg/m2 (5.2 lb/sq ft) Performance Maximum speed: 200 km/h (120 mph

Avro Antelope (456 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 22,000 ft (6,700 m) Rate of climb: 1,470 ft/min (7.5 m/s) Wing loading: 12 lb/sq ft (59 kg/m2) Power/mass: 0.106 hp/lb (0.174 kW/kg) Armament

Kawasaki Ki-5 (497 words) [view diff] exact match in snippet view article find links to article

(30,800 ft) Time to altitude: 5,000 metres (16,000 ft) in 8 minutes Wing loading: 103.9 kg/m2 (21.3 lb/sq ft) Power/mass: 0.35 kW/kg (0.21 hp/lb) Armament

Avia BH-25 (368 words) [view diff] exact match in snippet view article find links to article

altitude: 2,000 m (6,600 ft) in 16 minutes; 3,000 m (9,800 ft) in 30 minutes Wing loading: 46 kg/m2 (9.4 lb/sq ft) Power/mass: 0.1095 kW/kg (0.0666 hp/lb) Stroud

Lockheed L-649 Constellation (937 words) [view diff] exact match in snippet view article find links to article

3,685 km) with maximum payload Service ceiling: 24,442 ft (7,450 m) Wing loading: 57 lb/sq ft (280 kg/m2) Power/mass: 9.4 lb/hp (5.7 kg/kW) Aviation portal

Saro A.33 (357 words) [view diff] exact match in snippet view article find links to article

(280 km/h, 151 kn) Endurance: 12 hours Service ceiling: 14,280 ft (4,350 m) Wing loading: 34.8 lb/sq ft (170 kg/m2) Armament Guns: Machine guns in bow turret

Aeronca Arrow (303 words) [view diff] exact match in snippet view article find links to article

Range: 310 mi (500 km, 270 nmi) Rate of climb: 550 ft/min (2.8 m/s) Wing loading: 2.2 lb/sq ft (10.6 kg/m2) Power/mass: 15.9 lb/hp (9.65 kg/kW) Aircraft

Savoia-Marchetti SM.84 (2,770 words) [view diff] exact match in snippet view article find links to article

targets and many designs experienced problems with higher weights and wing loading than they were designed for. The SM.84 was far heavier than the SM.79

Ryan X-13 Vertijet (973 words) [view diff] exact match in snippet view article find links to article

Range: 192 mi (307 km, 167 nmi) Service ceiling: 20,000 ft (6,100 m) Wing loading: 35.2 lb/sq ft (172 kg/m2) Thrust/weight: 1.48 Aircraft of comparable

Douglas DF (551 words) [view diff] exact match in snippet view article find links to article

550 ft/min (2.8 m/s) at sea level 585 ft/min (2.97 m/s) at 5,000 ft (1,500 m) Wing loading: 22 lb/sq ft (110 kg/m2) Power/mass: 0.07 hp/lb (0.12 kW/kg) Wikimedia

Schleicher ASH 31 (456 words) [view diff] exact match in snippet view article find links to article

(retractable) Performance Rate of climb: 4 m/s (790 ft/min) Lift-to-drag: 56 Wing loading: 53.0 kg/m2 (10.8 lb/sq ft) max Aircraft of comparable role, configuration

Dornier Do 23 (633 words) [view diff] exact match in snippet view article find links to article

750 kg (19,290 lb) Time to altitude: 1,000 m (3,300 ft) in 4 minutes Wing loading: 85.2 kg/m2 (17.5 lb/sq ft) Power/mass: 0.12 kW/kg (0.073 hp/lb) Armament

Tachikawa Ki-55 (534 words) [view diff] exact match in snippet view article find links to article

900 ft) Time to altitude: 3,000 m (9,800 ft) in 6 minutes 55 seconds Wing loading: 86.1 kg/m2 (17.6 lb/sq ft) Power/mass: 0.222 kW/kg (0.135 hp/lb) Armament

Beardmore W.B.1a (173 words) [view diff] exact match in snippet view article find links to article

Cruise speed: 110 mph (180 km/h, 96 kn) Endurance: 6 hours 30 minutes Wing loading: 9.4 lb/sq ft (46 kg/m2) Power/mass: 0.058 hp/lb (0.095 kW/kg) Taylor

Aero A.100 (614 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 6,500 m (21,300 ft) Rate of climb: 4.2 m/s (830 ft/min) Wing loading: 73 kg/m2 (15 lb/sq ft) Power/mass: 0.170 kW/kg (0.103 hp/lb) Armament

Operation Sigma Sigma (1,051 words) [view diff] exact match in snippet view article find links to article

the wing area to 177 square feet (an increase of 35%), lowering the wing loading and stalling speed (37 knots), allowing the desired tight circling when

PZL.27 (548 words) [view diff] exact match in snippet view article find links to article

of climb: 4.6 m/s (910 ft/min) Time to altitude: 1,000m in 3min 37s Wing loading: 92.5 kg/m2 (18.9 lb/sq ft) Power/mass: 0.125 kW/kg Aircraft of comparable

Loire 102 (369 words) [view diff] exact match in snippet view article find links to article

000 m (13,120 ft) and 55% power Service ceiling: 6,000 m (20,000 ft) Wing loading: 135 kg/m2 (28 lb/sq ft) Related lists List of flying boats and floatplanes

Avia BH-26 (412 words) [view diff] exact match in snippet view article find links to article

000 ft) in 17 minutes 30 seconds; 7,000 m (23,000 ft) in 27 minutes Wing loading: 55.6 kg/m2 (11.4 lb/sq ft) Power/mass: 0.205 kW/kg (0.125 hp/lb) Armament

PZL.12 (495 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 4,200 m (13,800 ft) Rate of climb: 3.7 m/s (730 ft/min) Wing loading: 35 kg/m2 (7.2 lb/sq ft) Aircraft of comparable role, configuration,

Hongshanornis (1,380 words) [view diff] exact match in snippet view article find links to article

H. longicresta were broad and tapered, with an average wing area and wing loading compared to modern birds in the same size range. The presence or absence

Fokker D.XVII (701 words) [view diff] exact match in snippet view article find links to article

18 minutes to 8,000 m (26,000 ft) 29 minutes to 9,000 m (30,000 ft) Wing loading: 75 kg/m2 (15 lb/sq ft) Power/mass: 0.195 hp/lb (0.321 kW/kg) Armament

Tupolev TB-1 (913 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 4,830 m (15,850 ft) Rate of climb: 3.03 m/s (596 ft/min) Wing loading: 56.8 kg/m2 (11.6 lb/sq ft) Power/mass: 0.15 kW/kg (0.091 hp/lb) Armament

Backcountry Super Cubs Supercruiser (338 words) [view diff] exact match in snippet view article find links to article

Range: 580 mi (930 km, 500 nmi) Rate of climb: 1,000 ft/min (5.1 m/s) Wing loading: 14.1 lb/sq ft (69 kg/m2) Vandermeullen, Richard: 2012 Kit Aircraft Buyer's

ICA IAR-35 (489 words) [view diff] exact match in snippet view article find links to article

sink: 0.85 m/s (167 ft/min) *Minimum sink speed: 95 km/h (51 kn; 59 mph) Wing loading: 35.19 kg/m2 (7.21 lb/sq ft) Lambert, M. (1990). Jane's All the World's

PZL Bielsko SZD-50 Puchacz (619 words) [view diff] exact match in snippet view article find links to article

sink: 0.7 m/s (140 ft/min) *Minimum sink speed: 75 km/h (40 kn; 47 mph) Wing loading: 31.4 kg/m2 (6.4 lb/sq ft) Aircraft of comparable role, configuration

Civil Aviation Department MG-1 (502 words) [view diff] exact match in snippet view article find links to article

1.0 m/s (200 ft/min) minimum, at 90 km/h (56 mph; 49 kn), power off Wing loading: 34.3 kg/m2 (7.0 lb/sq ft) maximum Take-off run: 170 m (558 ft) Landing

Scheibe SF-26 Super Spatz (155 words) [view diff] exact match in snippet view article find links to article

110 kn) Rate of sink: 0.67 m/s (132 ft/min) at 89 km/h (48 kn; 55 mph) Wing loading: 25.2 kg/m2 (5.2 lb/sq ft) "Scheibe SF26". Taylor, Michael J. H. (1989)

Curtiss XP-71 (617 words) [view diff] exact match in snippet view article find links to article

000 m) Time to altitude: 25,000 ft (7,600 m) in 12 minutes 30 seconds Wing loading: 51.6 lb/sq ft (252 kg/m2) Power/mass: 0.147 hp/lb (0.242 kW/kg) Armament

Kawanishi E7K (705 words) [view diff] exact match in snippet view article find links to article

minutes Time to altitude: 3,000 m (9,800 ft) in 9 minutes 6 seconds Wing loading: 75.7 kg/m2 (15.5 lb/sq ft) Power/mass: 0.196 kW/kg (0.119 hp/lb) Armament

Blériot-SPAD S.56 (657 words) [view diff] exact match in snippet view article find links to article

Range: 620 km (390 mi, 330 nmi) Service ceiling: 4,800 m (15,700 ft) Wing loading: 52 kg/m2 (11 lb/sq ft) Power/mass: 0.1294 kW/kg (0.0787 hp/lb) Related

Avro 643 Cadet (891 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 12,000 ft (3,700 m) Rate of climb: 700 ft/min (3.6 m/s) Wing loading: 7.63 lb/sq ft (37.3 kg/m2) Power/mass: 0.075 hp/lb (0.123 kW/kg) Related

Lockheed XV-4 Hummingbird (609 words) [view diff] exact match in snippet view article find links to article

normal VTO range: 600 mi (966 km) Rate of climb: 12,000 ft/min (61 m/s) Wing loading: 69.2 lb/sq ft (338 kg/m2) Thrust/weight: 1.176 Aircraft of comparable

Kyushu K10W (674 words) [view diff] exact match in snippet view article find links to article

200 ft) Time to altitude: 5,000 m (16,000 ft) in 17 minutes 30 seconds Wing loading: 91.6 kg/m2 (18.8 lb/sq ft) Armament Guns: 1 × 7.7mm machine-gun Bombs:

Schleicher ASH 30 (466 words) [view diff] exact match in snippet view article find links to article

Performance Maximum glide ratio: >60 Rate of climb: 3 m/s (590 ft/min) Wing loading: 49.5 kg/m2 (10.1 lb/sq ft) Related lists List of gliders ASH 31 Mi serial

Slingsby T.53 (539 words) [view diff] exact match in snippet view article find links to article

Performance Maximum speed: 142 mph (228 km/h, 123 kn) Lift-to-drag: 30 Wing loading: 6.59 lb/sq ft (32.19 kg/m2) Related lists List of gliders List of aircraft

PZL S-1 (494 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 3,800 m (12,500 ft) Rate of climb: 3 m/s (590 ft/min) Wing loading: 60 kg/m2 (12 lb/sq ft) Related development Polikarpov Po-2 - PZL S-3

Ilyushin Il-103 (616 words) [view diff] exact match in snippet view article find links to article

4 / -1.8; Aerobatic: +6 / -3 Rate of climb: 3.167 m/s (623.4 ft/min) Wing loading: 89.1 kg/m2 (18.2 lb/sq ft) Power/mass: 8.37 kg/kW (13.75 lb/hp) Aircraft

Fairey Campania (840 words) [view diff] exact match in snippet view article find links to article

ceiling: 6,000 ft (1,800 m) Time to altitude: 2,000 ft (610 m) in 7 minutes Wing loading: 7.90 lb/sq ft (38.6 kg/m2) Power/mass: 0.049 hp/lb (0.081 kW/kg) Armament

Blériot-SPAD S.81 (523 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 8,000 m (26,000 ft) Rate of climb: 6 m/s (1,200 ft/min) Wing loading: 41.6 kg/m2 (8.5 lb/sq ft) Power/mass: 0.1787 kW/kg (0.1087 hp/lb) Armament

Blériot-SPAD S.81 (523 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 8,000 m (26,000 ft) Rate of climb: 6 m/s (1,200 ft/min) Wing loading: 41.6 kg/m2 (8.5 lb/sq ft) Power/mass: 0.1787 kW/kg (0.1087 hp/lb) Armament

Aichi E10A (486 words) [view diff] exact match in snippet view article find links to article

520 ft) Time to altitude: 3,000 m (9,800 ft) in 17 minutes 42 seconds Wing loading: 63.2 kg/m2 (12.9 lb/sq ft) Power/mass: 0.113 kW/kg (0.069 hp/lb) Armament

Republic XP-72 (726 words) [view diff] exact match in snippet view article find links to article

ceiling: 42,000 ft (12,805 m) Rate of climb: 5,280 ft/min (26.8 m/s) Wing loading: 48.1 lb/sq ft (235 kg/m2) Power/mass: 0.24 hp/lb (0.39 kW/kg) Armament

Albatros L103 (286 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 4,000 m (13,000 ft) Rate of climb: 2.7 m/s (530 ft/min) Wing loading: 44.12 kg/m2 (9.04 lb/sq ft) "Albatros Al 103". Germany. Archived from

Grigorovich MU-2 (243 words) [view diff] exact match in snippet view article find links to article

150 m (10,330 ft) Time to altitude: 1,000 m (3,300 ft) 10.8 minutes Wing loading: 30.9 kg/m2 (6.3 lb/sq ft) "MU-2 by D.P.Grigorovich". Ram-home.com. 1998-07-29

Caudron C.59 (573 words) [view diff] exact match in snippet view article find links to article

Maximum speed: 180 km/h (110 mph, 97 kn) Endurance: 3 hours 30 minutes Wing loading: 38.5 kg/m2 (7.9 lb/sq ft) Power/mass: 0.13476 kW/kg (0.08197 hp/lb)

Stolp SA-900 V-Star (596 words) [view diff] exact match in snippet view article find links to article

designed as a low-cost, economical and easy to fly design, with a light wing loading and short runway requirements. It features a strut-braced biplane layout

SZD-40x Halny (660 words) [view diff] exact match in snippet view article find links to article

modification from the original Zefir series wing was a change from Fowler (wing loading decreasing) flaps to camber increasing slotless flaps. This (flap) modification

Blohm & Voss Ha 140 (561 words) [view diff] exact match in snippet view article find links to article

(9,800 ft) in 11 minutes 30 seconds 5,000 m (16,000 ft) in 39 minutes Wing loading: 92.4 kg/m2 (18.9 lb/sq ft) Power/mass: 0.140 kW/kg (0.085hp/lb) Armament

Caudron C.140 (636 words) [view diff] exact match in snippet view article find links to article

100 kn) at 2,000 m (6,600 ft) Service ceiling: 5,000 m (16,000 ft) Wing loading: 46.5 kg/m2 (9.5 lb/sq ft) Power/mass: 0.13257 kW/kg (0.08064 hp/lb)

PZL.16 (544 words) [view diff] exact match in snippet view article find links to article

(120 mph, 110 kn) Range: 800 km (500 mi, 430 nmi) g limits: +7 ultimate Wing loading: 56 kg/m2 (11 lb/sq ft) Power/mass: 0.069 hp/lb (0.113 kW/kg) Related

Breda A.14 (323 words) [view diff] exact match in snippet view article find links to article

(50 mph, 43 kn) Endurance: 6h 30min Service ceiling: 5,000 m (16,000 ft) Wing loading: 44 kg/m2 (9.0 lb/sq ft) Power/mass: 0.1404 kW/kg (0.0854 hp/lb) Armament

Nakajima Ki-201 (504 words) [view diff] exact match in snippet view article find links to article

12,000 m (39,000 ft) Rate of climb: 12.9 m/s (2,540 ft/min) estimated Wing loading: 280 kg/m2 (57 lb/sq ft) Armament Guns: 2 × 30 mm (1.18 in) Ho-155 cannon

Consolidated NY (646 words) [view diff] no match in snippet view article find links to article

floats. The NY-2 had a longer span wing fitted to overcome the high wing-loading issue of the seaplane version. Tested with complete success during October

Blackburn Perth (513 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 11,500 ft (3,500 m) Rate of climb: 800 ft/min (4.1 m/s) Wing loading: 13.2 lb/sq ft (64 kg/m2) Power/mass: 0.076 hp/lb (0.125 kW/kg) Armament

Schleicher ASK 13 (542 words) [view diff] exact match in snippet view article find links to article

85 km/h (46 kn) Rate of sink: 0.80 m/s (157 ft/min) at 68 km/h (37 kn) Wing loading: 27.7 kg/m2 (5.7 lb/sq ft) Aircraft of comparable role, configuration

IS-4 Jastrząb (474 words) [view diff] exact match in snippet view article find links to article

47 kn) Rate of sink: 1.04 m/s (205 ft/min) at 70 km/h (43 mph; 38 kn) Wing loading: 29.7 kg/m2 (6.1 lb/sq ft) Aircraft of comparable role, configuration

Heinkel HD 22 (331 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 6,000 m (20,000 ft) Rate of climb: 4.5 m/s (890 ft/min) Wing loading: 48.8 kg/m2 (10.0 lb/sq ft) Power/mass: 0.1236 kW/kg (0.0752 hp/lb) Related

Valmet L-90 Redigo (612 words) [view diff] exact match in snippet view article find links to article

600 kg (3,500 lb) ISA 6.3 m/s (1,240 ft/min) @ 1,900 kg (4,200 lb) ISA Wing loading: 91.6 kg/m2 (18.8 lb/sq ft) Power/mass: 0.25 kW/kg (0.15 hp/lb) Armament

Backcountry Super Cubs Super Cub (349 words) [view diff] exact match in snippet view article find links to article

Range: 580 mi (930 km, 500 nmi) Rate of climb: 1,000 ft/min (5.1 m/s) Wing loading: 14.1 lb/sq ft (69 kg/m2) Vandermeullen, Richard: 2012 Kit Aircraft Buyer's

Avia B.35 (618 words) [view diff] exact match in snippet view article find links to article

Range: 500 km (311 mi, 270 nmi) Rate of climb: 13.0 m/s (2,560 ft/min) Wing loading: 129.41 kg/m2 (26.50 lb/sq ft) Aviation portal Related development Avia

Tachikawa Ki-70 (435 words) [view diff] exact match in snippet view article find links to article

000 m (36,000 ft) Time to altitude: 5,000 m (16,000 ft) in 5 minutes Wing loading: 229.2 kg/m2 (46.9 lb/sq ft) Power/mass: 0.288 kW/kg (0.175 hp/lb) Armament

IAR 14 (579 words) [view diff] exact match in snippet view article find links to article

900 ft) Time to altitude: 5,000 m (16,000 ft) in 10 minutes 27 seconds Wing loading: 76.5 kg/m2 (15.7 lb/sq ft) Power/mass: 0.217 kW/kg (0.132 hp/lb) Armament

Breda A.4 (368 words) [view diff] exact match in snippet view article find links to article

ceiling: 4,500 m (14,800 ft) landplane; 3,000 m (9,800 ft) seaplane Wing loading: 6.8 kg/m2 (1.4 lb/sq ft) Power/mass: 0.13 kW/kg (0.08 hp/lb) landplane;

Grigorovich MR-5 (242 words) [view diff] exact match in snippet view article find links to article

000 m (13,000 ft) Time to altitude: 1,000 m (3,281 ft) in 7.0 minutes Wing loading: 58.2 kg/m2 (11.9 lb/sq ft) Armament Guns: 1-2 x machine guns Шавров

Antonov A-15 (614 words) [view diff] exact match in snippet view article find links to article

0 kn) Rate of sink: 0.6 m/s (120 ft/min) at 90 km/h (55.9 mph; 48.6 kn) Wing loading: 31.6 kg/m2 (6.5 lb/sq ft) Related development Antonov A-9 Antonov A-11

Nakajima Type 91 fighter (580 words) [view diff] exact match in snippet view article find links to article

000 m (30,000 ft) Time to altitude: 3,000 m (9,800 ft) in 4 minutes Wing loading: 76.5 kg/m2 (15.7 lb/sq ft) Power/mass: 0.21 kW/kg (0.13 hp/lb) Armament

Heinkel He 71 (225 words) [view diff] exact match in snippet view article find links to article

speed: 160 km/h (99 mph, 86 kn) Range: 2,410 km (1,500 mi, 1,300 nmi) Wing loading: 52.3 kg/m2 (10.7 lb/sq ft) Power/mass: 0.115 Wikimedia Commons has media

Schleicher ASW 19 (585 words) [view diff] exact match in snippet view article find links to article

60 kn) Rate of sink: 0.55 m/s (108 ft/min) at 75 km/h (47 mph; 40 kn) Wing loading: 41.3 kg/m2 (8.5 lb/sq ft) maximum Aircraft of comparable role, configuration

Glaser-Dirks DG-200 (527 words) [view diff] exact match in snippet view article find links to article

270 km/h (168 mph, 146 kn) Stall speed: 62 km/h (39 mph, 33 kn) at 31 kg/m2 wing loading g limits: +5,3 -2,65 at manoeuvre speed Maximum glide ratio: 42 at 110

AAC SeaStar (304 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 12,000 ft (3,700 m) Rate of climb: 800 ft/min (4.1 m/s) Wing loading: 7.43 lb/sq ft (36.3 kg/m2) Related development AAC Seastar Sealoon EDRA

Slingsby Kite 2 (542 words) [view diff] exact match in snippet view article find links to article

87 kn) Stall speed: 54 km/h (34 mph, 29 kn) Maximum glide ratio: 23:1 Wing loading: 19.53 kg/m2 (4.00 lb/sq ft) Ellison 1971, p. 196 Ellison 1971, p. 261

Kawanishi Baika (628 words) [view diff] exact match in snippet view article find links to article

600 ft) Time to altitude: 3 minute 55 seconds to 2,000 m (6,600 ft) Wing loading: 188 kg/m2 (39 lb/sq ft) Thrust/weight: 0.2 Armament 1 × 250 kg (550

RWD 7 (531 words) [view diff] exact match in snippet view article find links to article

Range: 260 km (160 mi, 140 nmi) Service ceiling: 6,000 m (20,000 ft) Wing loading: 32 kg/m2 (6.6 lb/sq ft) Power/mass: 0.23 kW/kg (0.14 hp/lb) Take-off

LVG C.II (457 words) [view diff] exact match in snippet view article find links to article

(240 mi, 210 nmi) Endurance: 4 hours Service ceiling: 4,000 m (13,125 ft) Wing loading: 37 kg/m2 (7.6 lb/sq ft) Armament 1 × flexible 7.92 mm (.312 in) Parabellum

Albatros L 75 (337 words) [view diff] exact match in snippet view article find links to article

500 m (18,000 ft) Time to altitude: 1,000 m (3,300 ft) in 7 minutes Wing loading: 59.8 kg/m2 (12.2 lb/sq ft) Power/mass: 0.1141 kW/kg (0.0694 hp/lb) Grey

British Aerospace P.1233-1 Saba (309 words) [view diff] exact match in snippet view article find links to article

357 kW (4,502 hp) Performance Maximum speed: 740 km/h (460 mph, 400 kn) Wing loading: 242 kg/m2 (50 lb/sq ft) Takeoff distance: 300 m (1,000 ft) Armament

Bréguet 902 Cinzano (525 words) [view diff] exact match in snippet view article find links to article

42 kn) Rate of sink: 0.7 m/s (140 ft/min) at 65 km/h (40 mph; 35 kn) Wing loading: 23 kg/m2 (4.7 lb/sq ft) Cuny, Jean; Leyvastre, Pirre. Les Avions Breguet

Avro 571 Buffalo (485 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 13,700 ft (4,200 m) Rate of climb: 770 ft/min (3.9 m/s) Wing loading: 10.9 lb/sq ft (53 kg/m2) Power/mass: 0.071 hp/lb (0.117 kW/kg) Armament

Nakajima A4N (727 words) [view diff] exact match in snippet view article find links to article

390 ft) Time to altitude: 3,000 m (9,800 ft) in 3 minutes 30 seconds Wing loading: 76.9 kg/m2 (15.8 lb/sq ft) Power/mass: 0.2884 kW/kg (0.1754 hp/lb) Armament

Douglas XB-19 (1,209 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 23,000 ft (7,000 m) Rate of climb: 650 ft/min (3.3 m/s) Wing loading: 32.6 lb/sq ft (159 kg/m2) Power/mass: 0.057 hp/lb (0.094 kW/kg) Armament

Potez-CAMS 141 (698 words) [view diff] exact match in snippet view article find links to article

(160 mph, 140 kn) Endurance: 30 hours Service ceiling: 5,600 m (18,400 ft) Wing loading: 135 kg/m2 (28 lb/sq ft) Power/mass: 0.12 kW/kg (0.073 hp/lb) Armament

Aeros Still (279 words) [view diff] exact match in snippet view article find links to article

27 kn) Never exceed speed: 105 km/h (65 mph, 57 kn) g limits: +4/-2 Wing loading: 25.9 kg/m2 (5.3 lb/sq ft) maximum Bayerl, Robby; Martin Berkemeier;

Teichfuss Grifo (359 words) [view diff] exact match in snippet view article find links to article

glide ratio: estimated 17:1 Rate of sink: 0.9 m/s (180 ft/min) minimum Wing loading: 12.9 kg/m2 (2.6 lb/sq ft) Related lists List of gliders Pedrielli, Vincenzo;

BAT Baboon (432 words) [view diff] exact match in snippet view article find links to article

33 ft/min (4.2333 m/s) Time to altitude: 10,000 ft (3,048.0 m) in 12 minutes Wing loading: 5.2 lb/sq ft (25 kg/m2) Power/mass: 0.126 hp/lb (0.206 kW/kg) Aircraft

Bowlus SP-1 Paperwing (984 words) [view diff] exact match in snippet view article find links to article

low empty weight for its size of 160 lb (72.6 kg) and a matching low wing loading as well. Bowlus's lightweight construction techniques and design philosophies

Prometheus (spacecraft) (670 words) [view diff] exact match in snippet view article

2011-02-28. issues of volumetric efficiency, high L/D for cross range, low wing loading for reduced landing speed, and passive stability for all abort conditions

Potez-CAMS 141 (698 words) [view diff] exact match in snippet view article find links to article

(160 mph, 140 kn) Endurance: 30 hours Service ceiling: 5,600 m (18,400 ft) Wing loading: 135 kg/m2 (28 lb/sq ft) Power/mass: 0.12 kW/kg (0.073 hp/lb) Armament

Slingsby Falcon 4 (550 words) [view diff] exact match in snippet view article find links to article

weight: 775 lb (352 kg) Gross weight: 1,200 lb (544 kg) Performance Wing loading: 3.46 lb/sq ft (16.9 kg/m2) Ellison 1971, p. 194 Ellison 1971, pp. 172

Sparmann S-1 (337 words) [view diff] exact match in snippet view article find links to article

000 m (13,000 ft) in 14.7 minutes 5,000 m (16,000 ft) in 24.4 minutes Wing loading: 75 kg/m2 (15 lb/sq ft) normal; 70.2 kg/m2 (14.4 lb/sq ft) Power/mass:

Saro Shrimp (461 words) [view diff] exact match in snippet view article find links to article

(210 km/h, 110 kn) Endurance: 3 hours Rate of climb: 635 ft/min (3.23 m/s) Wing loading: 16.8 lb/sq ft (82 kg/m2) Aviation portal Related lists List of flying

Brochocki BKB-1 (816 words) [view diff] exact match in snippet view article find links to article

a very high wing area of 160 sq ft (15 m2) which resulted in a light wing loading of just 3.81 lb/sq ft (18.6 kg/m2). The prototype BKB-1 was originally

Schempp-Hirth Quintus (330 words) [view diff] no match in snippet view article find links to article

has a SOLO 2625-02i combustion engine. At 58 kg/m2 the Quintus has a wing-loading 20% higher than its predecessors and its high aspect ratio will give

Horten H.VII (436 words) [view diff] exact match in snippet view article find links to article

500 m (21,300 ft) Rate of climb: 7 m/s (1,400 ft/min) from sea level Wing loading: 45.5 kg/m2 (9.3 lb/sq ft) Power/mass: 5.7 kg/kW (9.4 lb/hp) Take-off:

Macchi M.41 (684 words) [view diff] exact match in snippet view article find links to article

500 m (24,600 ft) Time to altitude: 1,000 m (3,300 ft) in 2 minutes Wing loading: 48 kg/m2 (9.8 lb/sq ft) Power/mass: 0.196 kW/kg (0.119 hp/lb) Armament

Douglas O-46 (881 words) [view diff] exact match in snippet view article find links to article

ceiling: 24,150 ft (7,360 m) Rate of climb: 1,765 ft/min (8.97 m/s) Wing loading: 20 lb/sq ft (98 kg/m2) Power/mass: 1.087 hp/lb (1.787 kW/kg) Armament

Boeing XPBB Sea Ranger (1,105 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 22,400 ft (6,830 m) Rate of climb: 980 ft/min (4.98 m/s) Wing loading: 34.0 lb/sq ft (166 kg/m2) Power/mass: 0.15 hp/lb (0.24 kW/kg) Armament

Focke-Wulf A 20 Habicht (367 words) [view diff] exact match in snippet view article find links to article

000 m (3,300 ft) in 10 minutes A.20a 1,000 m (3,300 ft) in 5.4 minutes Wing loading: 44.5 kg/m2 (9.1 lb/sq ft) A.20a 50 kg/m2 (10 lb/sq ft)) Power/mass:

IS-5 Kaczka (622 words) [view diff] exact match in snippet view article find links to article

44 kn) Rate of sink: 1.26 m/s (248 ft/min) at 76 km/h (47 mph; 41 kn) Wing loading: 25.7 kg/m2 (5.3 lb/sq ft) Aircraft of comparable role, configuration

Backcountry Super Cubs Mackey SQ2 (349 words) [view diff] exact match in snippet view article find links to article

Range: 600 mi (970 km, 520 nmi) Rate of climb: 1,000 ft/min (5.1 m/s) Wing loading: 12.9 lb/sq ft (63 kg/m2) Vandermeullen, Richard: 2012 Kit Aircraft Buyer's

Miles Gemini (2,041 words) [view diff] exact match in snippet view article find links to article

of the more complex triple arrangement of the Messenger as the higher wing loading and elevated landing speed raised of the latter made the twin arrangement

Kawasaki Ki-56 (633 words) [view diff] exact match in snippet view article find links to article

000 m (26,000 ft) Time to altitude: 12 min 38 s to 3,000 m (9,800 ft) Wing loading: 156.7 kg/m2 (32.1 lb/sq ft) Power/mass: 0.184 kW/kg (0.112 hp/lb) Aircraft

Blériot 115 (434 words) [view diff] exact match in snippet view article find links to article

Range: 600 km (370 mi, 320 nmi) Service ceiling: 6,000 m (20,000 ft) Wing loading: 39 kg/m2 (8.0 lb/sq ft) Power/mass: 0.1088 kW/kg (0.0662 hp/lb) Wikimedia

Antonov A-13 (451 words) [view diff] exact match in snippet view article find links to article

60 kn) Rate of sink: 1.14 m/s (224 ft/min) at 97 km/h (60 mph; 52 kn) Wing loading: 34.5 kg/m2 (7.1 lb/sq ft) Related development Antonov A-9 Antonov A-11

Grigorovich MRL-1 (315 words) [view diff] exact match in snippet view article find links to article

050 m (10,010 ft) Time to altitude: 1,000 m (3,281 ft) in 11.0 minutes Wing loading: 52.0 kg/m2 (10.7 lb/sq ft) Armament Guns: 1-2 x machine guns Шавров

Siemens-Schuckert R.VIII (474 words) [view diff] exact match in snippet view article find links to article

490 nmi) (estimated) Service ceiling: 4,000 m (13,000 ft) (estimated) Wing loading: 35 kg/m2 (7.2 lb/sq ft) Cost 750,000 Marks Related development Siemens-Schuckert

Sopwith Snapper (635 words) [view diff] exact match in snippet view article find links to article

000 m) Time to altitude: 10,000 ft (3,000 m) in 7 minutes 50 seconds Wing loading: 7.5 lb/sq ft (37 kg/m2) Power/mass: 0.16 hp/lb (0.26 kW/kg) Armament

Vega Model 2 Starliner (883 words) [view diff] exact match in snippet view article find links to article

climb: 1,350 ft/min (6.9 m/s) 350 ft/min (1.8 m/s) on one engine half Wing loading: 20.3 lb/sq ft (99 kg/m2) Power/mass: 0.0869 hp/lb (0.1429 kW/kg) Aircraft

Granville Gee Bee Model A (1,556 words) [view diff] exact match in snippet view article find links to article

of climb Time to altitude: 10 minutes 0 seconds to 5,100 ft (1,600 m) Wing loading: 8.9 lb/sq ft (43 kg/m2) Power/mass: 16.5 lb/hp (10.0 kg/kW) Aviation

Beaujon Enduro (553 words) [view diff] exact match in snippet view article find links to article

Range: 250 mi (405 km, 220 nmi) Rate of climb: 350 ft/min (1.7 m/s) Wing loading: 4.2 lb/sq ft (20.8 kg/m2) Power/mass: 27.3 lb/hp (0.06 kW/kg) Aircraft

Schweizer X-26 Frigate (932 words) [view diff] exact match in snippet view article find links to article

aspect ratio: 18 Performance Maximum speed: 158 mph (254 km/h, 137 kn) Wing loading: 7.9 lb/sq ft (39 kg/m2) Power/mass: 0.07 hp/lb (0.12 kW/kg) Rate of

Renard R.17 (247 words) [view diff] exact match in snippet view article find links to article

000 m (13,000 ft) Time to altitude: 2,000 m (6,600 ft) in 12 minutes Wing loading: 50 kg/m2 (10 lb/sq ft) Power/mass: 16.9 lb/hp (10.3 kg/kW) Grey, C.G

BAT F.K.27 (366 words) [view diff] exact match in snippet view article find links to article

500 ft/min (13 m/s) Time to altitude: 5,000 ft (1,500 m) in 2 minutes Wing loading: 7 lb/sq ft (34 kg/m2) Power/mass: 0.143 hp/lb Grey, C.G. (1969). Jane's

Arado Ar 77 (636 words) [view diff] exact match in snippet view article find links to article

(937 ft/min) Time to altitude: 1,000 m (3,300 ft) in 3 minutes 30 seconds Wing loading: 57.2 kg/m2 (11.7 lb/sq ft) Power/mass: 0.166 PS/kg (0.122 kW/kg; 0.074 hp/lb)

Bristol Boarhound (687 words) [view diff] exact match in snippet view article find links to article

700 m) Time to altitude: 10,000 ft (3,048 m) in 10 minutes 38 seconds Wing loading: 9.61 lb/sq ft (46.9 kg/m2) Power/mass: 0.095 hp/lb (0.156 kW/kg) Armament

Tupolev Tu-14 (1,129 words) [view diff] exact match in snippet view article find links to article

550 nmi) Time to altitude: 5,000 m (16,000 ft) in 9 minutes 30 seconds Wing loading: 311 kg/m2 (64 lb/sq ft) Thrust/weight: 0.3 Take-off run: 1,200 m (3

Mitsubishi Ki-83 (753 words) [view diff] exact match in snippet view article find links to article

660 m (41,540 ft) Time to altitude: 10,000 m (33,000 ft) in 10 minutes Wing loading: 263 kg/m2 (54 lb/sq ft) Power/mass: 0.35 kW/kg (0.21 hp/lb) Armament

Piaggio PD.808 (758 words) [view diff] exact match in snippet view article find links to article

climb: 27.5 m/s (5,410 ft/min) at sea level and 7,176 kg (15,820 lb) Wing loading: 390.6 kg/m2 (80.0 lb/sq ft) Thrust/weight: 0.0036 kN/kg (0.37 lbf/lb)

Akaflieg Stuttgart fs32 (167 words) [view diff] exact match in snippet view article find links to article

57 kn) Rate of sink: 0.6 m/s (120 ft/min) at 85 km/h (53 mph; 46 kn) Wing loading: 50.3 kg/m2 (10.3 lb/sq ft) "fs32 – Aguila – Akaflieg Stuttgart e.V"

Teichfuss Balilla (384 words) [view diff] exact match in snippet view article find links to article

glide ratio: estimated 17:1 Rate of sink: 0.85 m/s (167 ft/min) minimum Wing loading: 11.6 kg/m2 (2.4 lb/sq ft) Related lists List of gliders Pedrielli, Vincenzo;

SZD-45 Ogar (692 words) [view diff] exact match in snippet view article find links to article

54 kn) Rate of sink: 0.96 m/s (189 ft/min) at 73 km/h (45 mph; 39 kn) Wing loading: 36.6 kg/m2 (7.5 lb/sq ft) Coates, Andrew (1980). Jane's World Sailplanes

Nakajima E4N (579 words) [view diff] exact match in snippet view article find links to article

Range: 1,019 km (633 mi, 550 nmi) Service ceiling: 5,740 m (18,830 ft) Wing loading: 60.7 kg/m2 (12.4 lb/sq ft) Power/mass: 0.24 kW/kg (0.15 hp/lb) Armament

Douglas Y1B-7 (1,349 words) [view diff] exact match in snippet view article find links to article

200 m) Time to altitude: 10,000 ft (3,000 m) in 8 minutes 42 seconds Wing loading: 16 lb/sq ft (78 kg/m2) Power/mass: 0.135 hp/lb (0.222 kW/kg) Armament

Yokosuka R2Y (461 words) [view diff] exact match in snippet view article find links to article

700 m (38,400 ft) Time to altitude: 10,000 m (33,000 ft) in 21 minutes Wing loading: 238.26 kg/m2 (48.80 lb/sq ft) Power/mass: 0.316 kW/kg (0.192 hp/lb)

Aichi S1A (479 words) [view diff] exact match in snippet view article find links to article

1,553 mi (2,500 km, 1,373 nmi) Service ceiling: 39,370 ft (12,000 m) Wing loading: 44.4 lb/sq ft (126.6 kg/m2) Armament Guns: 2× fuselage-mounted forward-firing

CEI Free Spirit Mk II (523 words) [view diff] exact match in snippet view article find links to article

has a very small wing area of 86.00 sq ft (7.990 m2), giving a high wing loading of 25.0 lb/sq ft (122 kg/m2). The cabin width is 44.5 in (113 cm). The

Hall Cherokee II (1,397 words) [view diff] exact match in snippet view article find links to article

ratio of 16.4:1, producing a wing area of 7 sq ft (0.65 m2) less and a wing loading 1 lb per sq ft higher. The wing uses a NACA 63(3)-618 laminar flow airfoil

Martin XB-33 Super Marauder (548 words) [view diff] exact match in snippet view article find links to article

2,000 mi (3,000 km, 1,700 nmi) Service ceiling: 39,000 ft (12,000 m) Wing loading: 58 lb/sq ft (280 kg/m2) Power/mass: 0.076 hp/lb (55 W/kg) Armament Guns:

Aero A.12 (358 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 7,500 m (24,600 ft) Rate of climb: 3.47 m/s (683 ft/min) Wing loading: 42 kg/m2 (8.6 lb/sq ft) Power/mass: 0.120 kW/kg (0.073 hp/lb) Armament

Aero A.200 (519 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 8,300 m (27,200 ft) Rate of climb: 1.5 m/s (300 ft/min) Wing loading: 57.2 kg/m2 (11.7 lb/sq ft) Take-off distance: 30 m (98 ft) Landing distance:

Martinsyde G.100 (820 words) [view diff] exact match in snippet view article find links to article

altitude: 10,000 ft (3,048 m) in 16 minutes with Beardmore 160 hp engine Wing loading: 5.2 lb/sq ft (25 kg/m2) Armament Guns: 1 × 0.303 in Lewis gun mounted

Aero A.200 (519 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 8,300 m (27,200 ft) Rate of climb: 1.5 m/s (300 ft/min) Wing loading: 57.2 kg/m2 (11.7 lb/sq ft) Take-off distance: 30 m (98 ft) Landing distance:

Yokosuka R2Y (461 words) [view diff] exact match in snippet view article find links to article

700 m (38,400 ft) Time to altitude: 10,000 m (33,000 ft) in 21 minutes Wing loading: 238.26 kg/m2 (48.80 lb/sq ft) Power/mass: 0.316 kW/kg (0.192 hp/lb)

Politechnika Warszawska PW-2 (482 words) [view diff] exact match in snippet view article find links to article

69 km/h (43 mph) Rate of sink: 1.1 m/s (220 ft/min) at 58 km/h (36 mph) Wing loading: 17.32 kg/m2 (3.55 lb/sq ft) Related lists List of gliders Puchalski

Bellanca CF (757 words) [view diff] exact match in snippet view article find links to article

speed: 35 kn (40 mph, 64 km/h) Rate of climb: 1,100 ft/min (5.6 m/s) Wing loading: 6.85 lb/sq ft (33.4 kg/m2) "Bellanca CF". Archived from the original

Yakovlev Yak-32 (670 words) [view diff] exact match in snippet view article find links to article

128 m (52,913 ft)) g limits: +7 -5 Rate of climb: 18 m/s (3,500 ft/min) Wing loading: 154 kg/m2 (32 lb/sq ft) Thrust/weight: 0.36 Take-off run: 425 m (1,394 ft)

Bonomi BS.15 Bigiarella (387 words) [view diff] exact match in snippet view article find links to article

Maximum glide ratio: 14:1 estimated Rate of sink: 0.74 m/s (146 ft/min) Wing loading: 13.10 kg/m2 (2.68 lb/sq ft) Pedrielli, Vincenzo; Camastra, Francesco

Westland Weasel (616 words) [view diff] exact match in snippet view article find links to article

700 ft (6,300 m) Time to altitude: 15,000 ft (4,572 m) in 19 minutes Wing loading: 8.35 lb/sq ft (40.8 kg/m2) Power/mass: 0.10 hp/lb (0.16 kW/kg) Armament

Aero A.104 (195 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 9,000 m (30,000 ft) Rate of climb: 6.8 m/s (1,340 ft/min) Wing loading: 88 kg/m2 (18 lb/sq ft) Power/mass: 0.21 kW/kg Armament Bombs: 200 kg

Zivko Edge 540 (435 words) [view diff] exact match in snippet view article find links to article

±10 540T solo Roll rate: 420°/sec Rate of climb: 3,700 ft/min (19 m/s) Wing loading: 12.4 lb/sq ft (61 kg/m2) empty 540T Aircraft of comparable role, configuration

Vought XF5U (1,156 words) [view diff] exact match in snippet view article find links to article

500 ft (10,516 m) Rate of climb: 3,120 ft/min (15.8 m/s) or 910 m/min Wing loading: 39.2 lb/sq ft (191 kg/m2) Armament 6 × .50 (12.7 mm) machine guns or

SZD-42 Jantar 2 (955 words) [view diff] exact match in snippet view article find links to article

(43 kn; 50 mph) Lift-to-drag: 50.3 maximum at 103 km/h (56 kn; 64 mph) Wing loading: 33.4 kg/m2 (6.8 lb/sq ft) without ballast 45.6 kg/m2 (9.34 lb/sq ft)

Douglas DT (648 words) [view diff] exact match in snippet view article find links to article

345 ft/min (1.75 m/s) Time to altitude: 14.5 min to 5,000 ft (1,524 m) Wing loading: 10.3 lb/sq ft (50 kg/m2) Power/mass: 0.0617 hp/lb (0.1 kW/kg) Armament

Sikorsky S-43 (1,450 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 19,000 ft (5,800 m) Rate of climb: 1,000 ft/min (5.1 m/s) Wing loading: 25 lb/sq ft (120 kg/m2) Power/mass: 13 lb/hp (7.9 kg/kW) Aviation portal

Blohm & Voss P 208 (674 words) [view diff] exact match in snippet view article find links to article

(30,000 ft) Endurance: 1.85 hr Service ceiling: 11,400 m (37,400 ft) Wing loading: 263 kg/m2 (54 lb/sq ft) List of German aircraft projects, 1939–45 Curtiss-Wright

RWD 3 (483 words) [view diff] exact match in snippet view article find links to article

speed: 140 km/h (87 mph, 76 kn) Stall speed: 68 km/h (42 mph, 37 kn) Wing loading: 37 kg/m2 (7.6 lb/sq ft) Related development RWD 2 RWD 4 RWD 7 Wikimedia

Fuji T-7 (582 words) [view diff] exact match in snippet view article find links to article

(3,002 ft) Stall speed: 104 km/h (65 mph, 56 kn) flaps and gear down Wing loading: 96.1 kg/m2 (19.7 lb/sq ft) Power/mass: 0.2114 kW/kg (0.1286 hp/lb) Take-off

Lavochkin-Gorbunov-Gudkov LaGG-1 (740 words) [view diff] exact match in snippet view article find links to article

(2,810 ft/min) Time to altitude: 5,000 m (16,000 ft) in 6.2 minutes Wing loading: 170 kg/m2 (35 lb/sq ft) Power/mass: 0.270 kW/kg (0.17 hp/lb) Armament

Grumman G-118 (578 words) [view diff] exact match in snippet view article find links to article

1,352 nmi (1,556 mi, 2,504 km) Service ceiling: 60,000 ft (18,288 m) Wing loading: 62.8 lb/sq ft (307 kg/m2) Armament Rockets: 2 x AIR-2 Genie unguided

Bell XFL Airabonita (1,106 words) [view diff] exact match in snippet view article find links to article

ceiling: 30,900 ft (9,400 m) Rate of climb: 2,630 ft/min (13.4 m/s) Wing loading: 29 lb/sq ft (140 kg/m2) Power/mass: 0.17 hp/lb (280 W/kg) Armament Guns:

Douglas DC-4 (1,933 words) [view diff] exact match in snippet view article find links to article

Ferry range: 4,250 mi (6,840 km, 3,690 nmi) with inner wing fuel cells Wing loading: 50.1 lb/sq ft (245 kg/m2) at maximum gross weight Power/mass: 0.0787 hp/lb

Blackburn Bluebird (614 words) [view diff] exact match in snippet view article find links to article

speed: 88 mph (142 km/h, 76 kn) Cruise speed: 70 mph (110 km/h, 61 kn) Wing loading: 5.83 lb/sq ft (28.5 kg/m2) Power/mass: 0.058 hp/lb (0.095 kW/kg) Related

Blohm & Voss P 209 (644 words) [view diff] exact match in snippet view article find links to article

540 nmi) Endurance: 1 to 1.5 hr Service ceiling: 12,000 m (39,000 ft) Wing loading: 285.0 kg/m2 (58.4 lb/sq ft) Sharp (2015) Masters (1982) Sharp (2017)

Kugisho B3Y (583 words) [view diff] exact match in snippet view article find links to article

Maximum speed: 219 km/h (136 mph, 118 kn) Endurance: 4 hours 30 minutes Wing loading: 64 kg/m2 (13 lb/sq ft) Power/mass: 0.14 kW/kg (0.085 hp/lb) Armament

SABCA S.2 (271 words) [view diff] exact match in snippet view article find links to article

speed: 80 km/h (50 mph; 43 kn) Service ceiling: 4,500 m (14,800 ft) Wing loading: 51.5 kg/m2 (10.5 lb/sq ft) Power/mass: 13.598 kg/kW (17.6 lb/hp) Taylor

Bréguet 280T (580 words) [view diff] exact match in snippet view article find links to article

altitude: 1,000 m (3,300 ft) in 6 minutes; 3,000 m (9,800 ft) in 29 minutes Wing loading: 55.5 kg/m2 (11.4 lb/sq ft) Power/mass: 0.1226 kW/kg (0.0746 hp/lb) Wikimedia

Polikarpov I-6 (913 words) [view diff] exact match in snippet view article find links to article

500 m (24,600 ft) Time to altitude: 5,000 m (16,000 ft) in 10 minutes Wing loading: 62 kg/m2 (13 lb/sq ft) Power/mass: 0.245 kW/kg (0.149 hp/lb) Horizontal

RWD 6 (731 words) [view diff] exact match in snippet view article find links to article

080 ft/min) Time to altitude: 1,000 m (3,300 ft) in 3 minutes 20 seconds Wing loading: 46.9 kg/m2 (9.6 lb/sq ft) Power/mass: 0.1522 kW/kg (.0926 hp/lb) Related

Avro 627 Mailplane (543 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 19,000 ft (5,800 m) Rate of climb: 1,200 ft/min (6.1 m/s) Wing loading: 13.5 lb/sq ft (66 kg/m2) Power/mass: 0.102 hp/lb (0.168 kW/kg) Related

DFS Kranich (839 words) [view diff] exact match in snippet view article find links to article

38 kn) Rate of sink: 0.7 m/s (140 ft/min) at 60 km/h (37 mph; 32 kn) Wing loading: 19.4 kg/m2 (4.0 lb/sq ft) aerokurier magazine 1/1999: Erich Klöckners

Lavochkin La-126 (597 words) [view diff] exact match in snippet view article find links to article

ceiling: 10,800 m (35,400 ft) Rate of climb: 17.8 m/s (3,500 ft/min) Wing loading: 188 kg/m2 (39 lb/sq ft) Power/mass: 0.42 kW/kg (0.26 hp/lb) Armament

LFG Roland D.VI (682 words) [view diff] exact match in snippet view article find links to article

790 m (19,000 ft) Time to altitude: 5,000 m (16,000 ft) in 19 minutes Wing loading: 38.3 kg/m2 (7.8 lb/sq ft) Power/mass: 0.18 kW/kg (0.11 hp/lb) Armament

Keystone Pronto (429 words) [view diff] exact match in snippet view article find links to article

30 seconds landplane; 10,000 ft (3,000 m) in 40 minutes floatplane; Wing loading: 9 lb/sq ft (44 kg/m2) landplane; 10.1 lb/sq ft (49 kg/m2) floatplane

Bristol Type 84 Bloodhound (588 words) [view diff] exact match in snippet view article find links to article

(210 km/h, 110 kn) Endurance: 3 hours Service ceiling: 22,000 ft (6,700 m) Wing loading: 8.57 lb/sq ft (41.8 kg/m2) Power/mass: 0.10 hp/lb (0.16 kW/kg) Armament

Fieseler Fi 99 (412 words) [view diff] exact match in snippet view article find links to article

in 7 minutes 30 seconds 3,000 m (9,800 ft) in 12 minutes 30 seconds Wing loading: 51.45 kg/m2 (10.54 lb/sq ft) Power/mass: 0.183 PS/m2 (0.017 hp/sq ft;

Latécoère 25 (478 words) [view diff] exact match in snippet view article find links to article

200 m (13,800 ft) Time to altitude: 4,000 m (13,000 ft) in 44 minutes Wing loading: 67.5 kg/m2 (13.8 lb/sq ft) Power/mass: 0.1027 kW/kg (0.0625 hp/lb) Wikimedia

Westland C.O.W. Gun Fighter (438 words) [view diff] exact match in snippet view article find links to article

400 ft (8,961 m) Time to altitude: 10,000 ft (3,048 m) in 7 minutes Wing loading: 17.4 lb/sq ft (85 kg/m2) Power/mass: 0.12 hp/lb (0.20 kW/kg) Armament

Teichfuss Tenax (452 words) [view diff] exact match in snippet view article find links to article

weight: 210 kg (463 lb) Performance Maximum glide ratio: estimated 17:1 Wing loading: 13 kg/m2 (2.7 lb/sq ft) Related lists List of gliders Pedrielli, Vincenzo;

Blackburn B-3 (548 words) [view diff] exact match in snippet view article find links to article

150 ft (2,790 m) Time to altitude: 6,500 ft (1,981 m) in 20 minutes Wing loading: 16 lb/sq ft (78 kg/m2) Power/mass: 0.079 hp/lb (0.130 kW/kg) Armament

Schleicher Ka 3 (535 words) [view diff] exact match in snippet view article find links to article

weight: 100 kg (220 lb) equipped Max takeoff weight: 195 kg (430 lb) Wing loading: 19.7 kg/m2 (4.04 lb/sq ft) maximum Performance Maximum speed: 160 km/h

Teichfuss Falco (424 words) [view diff] exact match in snippet view article find links to article

ratio: estimated 21.5:1 Rate of sink: 0.65 m/s (128 ft/min) minimum Wing loading: 12.9 kg/m2 (2.6 lb/sq ft) Related lists List of gliders Pedrielli, Vincenzo;

Rumpler C.I (647 words) [view diff] exact match in snippet view article find links to article

at sea level Endurance: 4 hours Service ceiling: 5,050 m (16,570 ft) Wing loading: 36 kg/m2 (7.4 lb/sq ft) Armament Aircraft of comparable role, configuration

W.A.R. P-51 Mustang (265 words) [view diff] exact match in snippet view article find links to article

Stall speed: 48 kn (55 mph, 89 km/h) Range: 350 nmi (400 mi, 640 km) Wing loading: 12 lb/sq ft (59 kg/m2) Aircraft of comparable role, configuration, and

CAC CA-15 (1,293 words) [view diff] exact match in snippet view article find links to article

(25 m/s) Time to altitude: 20,000 ft (6,100 m) in 5 minutes 30 seconds Wing loading: 37.5 lb/sq ft (183 kg/m2) normal load 48.8 lb/sq ft (238.3 kg/m2) Power/mass:

Teichfuss Borea (389 words) [view diff] exact match in snippet view article find links to article

ratio: estimated 32.5:1 Rate of sink: 0.65 m/s (128 ft/min) minimum Wing loading: 24.7 kg/m2 (5.1 lb/sq ft) Related lists List of gliders Pedrielli, Vincenzo;

Schleicher ASH 26 (466 words) [view diff] exact match in snippet view article find links to article

48 m/s (94 ft/min) and 1.75 m/s (5.7 ft/s) at 200 km/h (120 mph; 110 kn) Wing loading: 45 kg/m2 (9.2 lb/sq ft) "Dipl.-Ing. Martin Heide has retired". Alexander

Westland Wagtail (696 words) [view diff] exact match in snippet view article find links to article

(3,000 m) in 7 minutes 30 seconds; 17,000 ft (5,200 m) in 17 minutes Wing loading: 7 lb/sq ft (34 kg/m2) Power/mass: 0.13 hp/lb (0.213 kW/kg) Armament

Curtiss XP-62 (666 words) [view diff] exact match in snippet view article find links to article

500 ft (11,400 m) Time to altitude: 15,000 ft (4,600 m) in 6.9 minutes Wing loading: 35 lb/sq ft (170 kg/m2) Power/mass: 0.16 hp/lb (0.26 kW/kg) Armament

Schreder HP-19 (302 words) [view diff] exact match in snippet view article find links to article

mph (80 km/h) Rate of sink: 96 ft/min (0.49 m/s) at 40 mph (64 km/h) Wing loading: 8.58 lb/sq ft (41.9 kg/m2) List of gliders Activate Media (2006). "HP-19

Rutan Solitaire (640 words) [view diff] exact match in snippet view article find links to article

Performance Maximum glide ratio: 32:1 Rate of sink: 150 ft/min (0.76 m/s) Wing loading: 6.05 lb/sq ft (29.5 kg/m2) List of gliders "J2mcL Planeurs - Fiche planeur

Lioré et Olivier LeO H-10 (367 words) [view diff] exact match in snippet view article find links to article

300 ft) estimated Service ceiling: 5,550 m (18,210 ft) service, estimated Wing loading: 42 kg/m2 (8.6 lb/sq ft) Power/mass: 0.07 hp/lb (110 W/kg) "The Paris

Schreder HP-19 (302 words) [view diff] exact match in snippet view article find links to article

mph (80 km/h) Rate of sink: 96 ft/min (0.49 m/s) at 40 mph (64 km/h) Wing loading: 8.58 lb/sq ft (41.9 kg/m2) List of gliders Activate Media (2006). "HP-19

Levasseur PL.4 (444 words) [view diff] exact match in snippet view article find links to article

000 m (16,000 ft) Time to altitude: 3,000 m (9,800 ft) in 20 minutes Wing loading: 43 kg/m2 (8.8 lb/sq ft) Power/mass: 0.1337 kW/kg (0.0813 hp/lb) Armament

Embraer EMB 400 Urupema (486 words) [view diff] exact match in snippet view article find links to article

best 36:1 at 95 km/h; 52 kn (59 mph) Rate of sink: 0.66 m/s (78 ft/min) Wing loading: 25.83 kg/m2 (5.29 lb/sq ft) maximum List of Brazilian gliders Aircraft

Teichfuss Turbine (436 words) [view diff] exact match in snippet view article find links to article

glide ratio: estimated 33:1 Rate of sink: 0.54 m/s (106 ft/min) minimum Wing loading: 21.0 kg/m2 (4.3 lb/sq ft) Related lists List of gliders Pedrielli, Vincenzo;

SZD-6X Nietoperz (1,028 words) [view diff] exact match in snippet view article find links to article

49 kn) Rate of sink: 1.35 m/s (266 ft/min) at 80 km/h (50 mph; 43 kn) Wing loading: 18.7 kg/m2 (3.8 lb/sq ft) Aircraft of comparable role, configuration

Schempp-Hirth Discus-2 (610 words) [view diff] exact match in snippet view article find links to article

110 kn) Maximum glide ratio: 42 Rate of sink: 0.59 m/s (116 ft/min) Wing loading: 30.7–51.7 kg/m2 (6.3–10.6 lb/sq ft) Aircraft of comparable role, configuration

SZD-25A Lis (909 words) [view diff] exact match in snippet view article find links to article

Lis) 0.9 m/s (177.2 ft/min) at 60 km/h (37.3 mph; 32.4 kn) (SZD-16 Gil) Wing loading: 24.7 kg/m2 (5.1 lb/sq ft) (SZD-25A Lis) 21.3 kg/m2 (4.36 lb/sq ft) (SZD-16

Albatros L.71 (590 words) [view diff] exact match in snippet view article find links to article

67 kn) at sea level Time to altitude: 12 min to 1,000 m (3,280 ft) Wing loading: 26.3 kg/m2 (5.38 lb/sq ft) Power/mass: 0.038 hp/lb (62 W/kg) Throughout

Scheibe SF 32 (249 words) [view diff] exact match in snippet view article find links to article

(390 ft/min) Rate of sink: 0.65 m/s (128 ft/min) at 80 km/h (43 kn; 50 mph) Wing loading: 33.8 kg/m2 (6.9 lb/sq ft) Take-off run: 200 m (660 ft) "Scheibe SF27

Howard DGA-15 (1,254 words) [view diff] exact match in snippet view article find links to article

exceeding airline standards with limousine-like capaciousness, and high wing loading allowing the Howards to ride through most turbulence comfortably. Prior

Bristol Primary Trainer (549 words) [view diff] exact match in snippet view article find links to article

fixed-pitch propeller Performance Maximum speed: 96 mph (154 km/h, 83 kn) Wing loading: 6.69 lb/sq ft (32.7 kg/m2) Barnes, C.H. (1964). Bristol Aircraft Since

Bushcaddy L-160 (420 words) [view diff] exact match in snippet view article find links to article

(4,000 m) g limits: +5.3/-3.2 Rate of climb: 1,300 ft/min (6.6 m/s) Wing loading: 11.64 lb/sq ft (56.8 kg/m2) Vandermeullen, Richard: 2012 Kit Aircraft

Mikoyan-Gurevich MiG-105 (714 words) [view diff] exact match in snippet view article find links to article

Performance Maximum speed: 800 km/h (500 mph, 430 kn) Maximum speed: Mach 0.65 Wing loading: 175 kg/m2 (36 lb/sq ft) Landing speed: 250–270 km/h (160–170 mph; 130–150 kn)

Handley Page HP.14 (406 words) [view diff] exact match in snippet view article find links to article

700 m) Time to altitude: 10,000 ft (3,048 m) in 29 minutes 30 seconds Wing loading: 7.67 lb/sq ft (37.4 kg/m2) Power/mass: 0.067 hp/lb (0.110 kW/kg) Armament

Caproni Vizzola 2 (535 words) [view diff] exact match in snippet view article find links to article

glide ratio: estimated 21:1 Rate of sink: 0.73 m/s (144 ft/min) minimum Wing loading: 19 kg/m2 (3.9 lb/sq ft) Pedrielli, Vincenzo; Camastra, Francesco (2011)

RWD 16 (591 words) [view diff] exact match in snippet view article find links to article

620 ft) Time to altitude: 1,000 m (3,300 ft) in 6 minutes 30 seconds Wing loading: 41.5 kg/m2 (8.5 lb/sq ft) Power/mass: 0.0768 kW/kg (0.0467 hp/lb) Glass

Bonomi BS.10 Ardea (419 words) [view diff] exact match in snippet view article find links to article

Maximum glide ratio: 26:1 estimated Rate of sink: 0.53 m/s (104 ft/min) Wing loading: 12.50 kg/m2 (2.56 lb/sq ft) Pedrielli, Vincenzo; Camastra, Francesco

Velocity SE (424 words) [view diff] exact match in snippet view article find links to article

000 ft (6,100 m) g limits: +12 -7 Rate of climb: 1,200 ft/min (6.1 m/s) Wing loading: 18.88 lb/sq ft (92.2 kg/m2) Velocity XL Raptor Aircraft Raptor Rutan

Union G.I (536 words) [view diff] exact match in snippet view article find links to article

194 m/s (235.0 ft/min) Time to altitude: 1,500 m. (4,921 ft.) in 24.2 min Wing loading: 38.2 kg/m2 (7.8 lb/sq ft) Aircraft of comparable role, configuration

IAR-46 (377 words) [view diff] exact match in snippet view article find links to article

(16,000 ft) g limits: +4.4, -2.2 Rate of climb: 4.30 m/s (846 ft/min) Wing loading: 54.1 kg/m2 (11.1 lb/sq ft) Power/mass: 12.58 kg/kW (20.67 lb/hp) Jackson

Advanced Aeromarine Sierra (352 words) [view diff] exact match in snippet view article find links to article

27 mph (43 km/h, 23 kn) Maximum glide ratio: 25:1 at 40 mph (64 km/h) Wing loading: 3.2 lb/sq ft (16 kg/m2) Related development Moyes Tempest Aircraft of

Győr-2 (1,222 words) [view diff] exact match in snippet view article find links to article

achieved through Göppingen type airbrakes on upper and lower wing surfaces. Wing loading could also be adjusted on the ground by attaching ballast to the wing

PZL.44 Wicher (702 words) [view diff] exact match in snippet view article find links to article

engine ceiling: 2,300 m (7,500 ft) Rate of climb: 6.93 m/s (1,365 ft/min) Wing loading: 123.5 kg/m2 (25.3 lb/sq ft) Power/mass: 0.138 kW/kg (0.084 hp/lb) Aircraft

Douglas DC-4E (982 words) [view diff] exact match in snippet view article find links to article

ceiling: 22,900 ft (7,000 m) Rate of climb: 1,175 ft/min (5.97 m/s) Wing loading: 28.5 lb/sq ft (139 kg/m2) Power/mass: 0.0943 hp/lb (4.8kW/kg) Related

Sopwith B.1 (782 words) [view diff] exact match in snippet view article find links to article

800 m) Time to altitude: 10,000 ft (3,048 m) in 15 minutes 30 seconds Wing loading: 6.64 lb/sq ft (32.4 kg/m2) Power/mass: 0.065 hp/lb (0.107 kW/kg) Armament

Dassault Mirage 4000 (770 words) [view diff] exact match in snippet view article find links to article

(60,000 ft/min) Time to altitude: 15,000 m (49,000 ft) (M2) 3 minutes Wing loading: 220 kg/m2 (45 lb/sq ft) at combat weight Thrust/weight: 1.2 Armament

Aerosport Quail (260 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 12,000 ft (3,700 m) Rate of climb: 820 ft/min (4.2 m/s) Wing loading: 8.92 lb/sq ft (43.6 kg/m2) Wikimedia Commons has media related to Aerosport

Fisher FP-505 Skeeter (580 words) [view diff] exact match in snippet view article find links to article

speed: 83 mph (134 km/h, 72 kn) Rate of climb: 800 ft/min (4.1 m/s) Wing loading: 4.5 lb/sq ft (21.95 kg/m2) Power/mass: 10.0 lb/hp (0.16 kW/kg) Aircraft

Schreder HP-17 (326 words) [view diff] exact match in snippet view article find links to article

ratio: 40:1 Rate of sink: 102 ft/min (0.52 m/s) at 40 mph (64 km/h) Wing loading: 8.3 lb/sq ft (41 kg/m2) with full water ballast List of gliders Said

Antonov A-11 (738 words) [view diff] exact match in snippet view article find links to article

4 kn) Rate of sink: 0.74 m/s (146 ft/min) at 86 km/h (53.4 mph; 46.4 kn) Wing loading: 33 kg/m2 (6.8 lb/sq ft) Wikimedia Commons has media related to Antonov

Daimler G.I (704 words) [view diff] exact match in snippet view article find links to article

climb: 1.1 m/s (220 ft/min) Time to altitude: 1,500m (4,921ft) in 25 min Wing loading: 49.3 kg/m2 (10.1 lb/sq ft) Aircraft of comparable role, configuration

Laville DI-4 (322 words) [view diff] exact match in snippet view article find links to article

440 m (21,130 ft) Time to altitude: 5,000 m (16,000 ft) in 17 minutes Wing loading: 81.5 kg/m2 (16.7 lb/sq ft) Power/mass: 0.230 kW/kg (0.140 hp/lb) Horizontal

Aichi H9A (554 words) [view diff] exact match in snippet view article find links to article

(890 ft/min) Time to altitude: 3,000 m (9,800 ft) in 11 minutes 14 seconds Wing loading: 110.6 kg/m2 (22.7 lb/sq ft) Power/mass: 0.151 kW/kg (0.092 hp/lb) Armament

Hawker Henley (1,126 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 27,000 ft (8,200 m) Rate of climb: 1,150 ft/min (5.8 m/s) Wing loading: 25.9 lb/sq ft (126 kg/m2) Power/mass: 0.12 hp/lb (0.20 kW/kg) Related

Schempp-Hirth Nimbus-3 (512 words) [view diff] exact match in snippet view article find links to article

59 mph) Rate of sink: 0.44 m/s (87 ft/min) at 75 km/h (40 kn; 47 mph) Wing loading: 46 kg/m2 (9.4 lb/sq ft) Aircraft of comparable role, configuration,

Schleicher ASK 21 (1,135 words) [view diff] exact match in snippet view article find links to article

90 km/h (49 kn) Rate of sink: 0.64 m/s (126 ft/min) at 67 km/h (36 kn) Wing loading: 33.4 kg/m2 (6.8 lb/sq ft) IS 28 B2 Schleicher ASK 23 ZS Jezow PW-6U

Schneider ES-65 (545 words) [view diff] exact match in snippet view article find links to article

72 km/h (45 mph, 39 kn) Never exceed speed: 260 km/h (160 mph, 140 kn) Wing loading: 36.4 kg/m2 (7.5 lb/sq ft) Wikimedia Commons has media related to Schneider

Farman F.200 (1923) (718 words) [view diff] exact match in snippet view article

Range: 400 km (250 mi, 220 nmi) Service ceiling: 3,200 m (10,500 ft) Wing loading: 40 kg/m2 (8.2 lb/sq ft) Landing speed: 70 km/h (43 mph) Serryer, J (5

Piper PA-12 Super Cruiser (889 words) [view diff] exact match in snippet view article find links to article

(absolute) at 1,550 lb (700 kg) Rate of climb: 510 ft/min (2.6 m/s) Wing loading: 9.76 lb/sq ft (47.7 kg/m2) Take-off Run: 480 ft (150 m) at 1,550 lb

Messerschmitt M 18 (610 words) [view diff] exact match in snippet view article find links to article

1 m/s (610 ft/min) Time to altitude: 1,000 m (3,281 ft) in 7 minutes Wing loading: 75 kg/m2 (15 lb/sq ft) Power/mass: 0.126 kW/kg (0.077 hp/lb) Wikimedia

PZL Krosno KR-03 Puchatek (470 words) [view diff] exact match in snippet view article find links to article

ratio: 27:1 at 88 km/h (55 mph) Rate of sink: 0.78 m/s (154 ft/min) Wing loading: 27.78 kg/m2 (5.69 lb/sq ft) Related lists List of gliders Activate Media

Lancair 360 (235 words) [view diff] exact match in snippet view article find links to article

510–640 nmi (580–730 mi, 940–1,180 km) (75%, std/opt fuel) g limits: +9.0 -4.5 Wing loading: 22.17 lb/sq ft (108.2 kg/m2) Power/mass: 0.107 Wikimedia Commons has

Warsztaty Szybowcowe Orlik (585 words) [view diff] exact match in snippet view article find links to article

(561 lb) Performance Maximum glide ratio: 26.5:1 at 71 km/h (44 mph) Wing loading: 16.8 kg/m2 (3.44 lb/sq ft) Related lists List of gliders Activate Media

Savoia-Marchetti SM.83 (791 words) [view diff] exact match in snippet view article find links to article

(9,843 ft) in 9 minutes 4,000 m (13,123 ft) in 13 minutes 30 seconds Wing loading: 169 kg/m2 (35 lb/sq ft) Power/mass: 0.173 kW/kg (0.1 hp/lb) Related

IVL C.24 (256 words) [view diff] exact match in snippet view article find links to article

180 kW (240 hp) Performance Maximum speed: 200 km/h (120 mph, 110 kn) + Wing loading: 44.7 kg/m2 (9.2 lb/sq ft) Related lists List of aircraft of the Finnish

Fuji T-3 (511 words) [view diff] exact match in snippet view article find links to article

Service ceiling: 8,170 m (26,800 ft) Rate of climb: 7.7 m/s (1,520 ft/min) Wing loading: 91.5 kg/m2 (18.7 lb/sq ft) Japan portal Aviation portal Related development

Slingsby Skylark (602 words) [view diff] exact match in snippet view article find links to article

37 kn (69 km/h; 43 mph) Lift-to-drag: 27:1 at 42 kn (78 km/h; 48 mph) Wing loading: 5.9 lb/sq ft (28.8 kg/m2) Aircraft of comparable role, configuration

PZL-105 Flaming (740 words) [view diff] exact match in snippet view article find links to article

limits: +3.8 -1.52 Rate of climb: 5.5 m/s (1,080 ft/min) at sea level Wing loading: 109.5 kg/m2 (22.4 lb/sq ft) Power/mass: 0.145 kW/kg (0.088 hp/lb) Take-off:

Savoia-Marchetti SM.62 (1,047 words) [view diff] exact match in snippet view article find links to article

200 m (13,800 ft) Time to altitude: 3,000 m (9,800 ft) in 24 minutes Wing loading: 46.15 kg/m2 (9.45 lb/sq ft) Power/mass: 0.125 kW/kg (0.076 hp/lb) Armament