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alternate case: thrust

Roger Moore (9,228 words) [view diff] exact match in snippet view article find links to article

in Curse of the Pink Panther (1983) (for which he was credited as "Turk Thrust II"). Then he tried a thriller The Naked Face (1984), written and directed

The pelvic thrust is the thrusting motion of the pelvic region, which is used for a variety of activities, such as dance, exercise, or sexual activity

fault-bend fold diagram. Thrust faults form nappes and klippen in the large thrust belts. Subduction zones are a special class of thrusts that form the largest

A thrust fault is a break in the Earth's crust, across which older rocks are pushed above younger rocks. A thrust fault is a type of reverse fault that

include a variety of types of aircraft including helicopters as well as thrust-vectoring fixed-wing aircraft and other hybrid aircraft with powered rotors

0 flew from 2010 to 2013, v1.1 flew from 2013 to 2016, while v1.2 Full Thrust first launched in 2015, encompassing the Block 5 variant, which has been

legs into position for the thrust phase, and move very fast during the thrust phase. Again, the goal is to produce maximum thrust during the insweep phase

forced underneath another. The earthquakes are caused by slip along the thrust fault that forms the contact between the two plates. These interplate earthquakes

siciliano (Sicilian school of stiletto fighting). The stiletto was purely a thrusting or stabbing weapon, and the scherma di stiletto siciliano accordingly

by the Komsomolsk-on-Amur Aircraft Production Association before having thrust-vectoring nozzles installed. It also had updated flight- and weapons-control

continental end of passive margin sequences where a detachment layer is present. Thrust tectonics is associated with the shortening and thickening of the crust

Canada VZ-9 Avrocar (ducted fan) BAE Harrier II (vectored thrust) BAE Sea Harrier (vectored thrust) Bell 65 ATV (Tiltjet) Bell/Agusta BA609 (tiltrotor), presently

geology, a nappe or thrust sheet is a large sheetlike body of rock that has been moved more than 2 km (1.2 mi) or 5 km (3.1 mi) above a thrust fault from its

Beast Wars: Transformers (titled Beasties: Transformers in Canada) is an animated television series that debuted on September 16, 1996 and ended on May

eliminates the need for a separate hydraulic drive system and means that thrust vectoring control failure by running out of hydraulic fluid is not possible

and thrust belt (FTB) is a series of mountainous foothills adjacent to an orogenic belt, which forms due to contractional tectonics. Fold and thrust belts

providing 4846  kN of thrust. Within T+1, 4 out of the 6 boosters ignite on ground, each producing 703 kN of thrust. 7658 kN of total thrust is produced by the

Abdominal thrusts, also known as the Heimlich maneuver or Heimlich manoeuvre, is a first-aid procedure used to treat upper-airway obstructions (or choking)

In theatre, a thrust stage (a platform stage or open stage) is one that extends into the audience on three sides and is connected to the backstage area

tailplanes (horizontal or vertical). Attitude control would rely purely on 3D thrust vectoring. The aircraft design was derived from the F-22 Raptor and featured

Operation Mameluke Thrust was a US Marine Corps operation that took place in Happy Valley southwest of Danang, lasting from 19 May to 23 October 1968.

usually a ship on a waterway. This type is sometimes referred to as a thrust bridge. Retractable bridges date back to medieval times. Due to the large

the thrust of the mass above, transferring it from stone to stone to the springer's bottom face (impost), which is horizontal and passes the thrust on

fabricate. The compete-on-cost strategy also led Boeing to pick a direct-lift thrust vectoring system, for the Marines' short take-off and vertical landing (STOVL)

S125/S139 solid rocket booster and the liquid-fueled Vikas engine. Due to the thrust required for injecting the satellite in a geostationary transfer orbit (GTO)

rolling takeoff, sometimes with a ramp (ski-jump), reduces the amount of thrust required to lift an aircraft from the ground (compared with vertical takeoff)

the remaining sides hidden and used by the performers and technicians. Thrust stages may be similar to proscenium stages but with a platform or performance

Thrust tectonics or contractional tectonics is concerned with the structures formed by, and the tectonic processes associated with, the shortening and

gas-generator cycle. The engine produces a nominal thrust of 200 kN, but has an operating thrust range between 180 kN to 220 kN and can be set to any

regional airliners Thrust engines, excluding auxiliary power units or other turbines which do not provide significant aircraft thrust As of July 2020; on-order

least drag, which requires correct diver trim. Efficient production of thrust also reduces the effort required, but there are also situations where efficiency

there is an outward thrust generated against the walls underneath a barrel vault. There are several mechanisms for absorbing this thrust. One is to make the

Twelfth Night, or What You Will is a romantic comedy by William Shakespeare, believed to have been written around 1601–1602 as a Twelfth Night entertainment

of several ranges that constitute the Maria Fold and Thrust Belt (MFTB). The Maria Fold and Thrust Belt underwent generally thick-skinned (involving basement

earliest versions, developed in 1965, had a sea-level thrust of about 190 kN. By 1971, the thrust had improved to 540 kN, with resulting engine named Viking

test pilots. The NF-16D VISTA testbed aircraft incorporated a multi-axis thrust vectoring (MATV) engine nozzle that provides for more active control of

Medium+ versions. At lift-off, all three rocket engines would operate at full thrust, and 44 seconds later the central engine would throttle down to 55% to conserve

system with 360,000 pounds-force (1,600 kN) of thrust versus the 250,000 pounds-force (1,100 kN) of thrust in the Atlas B/C's engines. Operational Atlas

transferring the weight of the bridge and its loads partially into a horizontal thrust restrained by the abutments at either side, and partially into a vertical

Jetstorm Paul Dobson as Tankor, Obsidian, Diagnostic Drone #2 Jim Byrnes as Thrust Alessandro Juliani as Nightscream Richard Newman as Rhinox/Tankor Kathleen

Operation Mountain Thrust was a joint NATO and Afghan-led military operation in the War in Afghanistan. It involved more than 3,300 British troops, 2,300

Jetstorm Paul Dobson as Tankor, Obsidian, Diagnostic Drone #2 Jim Byrnes as Thrust Alessandro Juliani as Nightscream Richard Newman as Rhinox/Tankor Kathleen

or thrust of an aircraft. The EWR VJ 101 used tip mounted jets, the V-22 uses tilting wingtip mounted engines, and the Harrier uses wingtip thrust for

crash was attributed to pilot error. While the captain was reducing the thrust reverser of the right engine, he unintentionally moved the left engine's

faults, thrusts or thrust faults and strike-slip faults. Many faults may have acted as both normal faults at one time and as reverse or thrust faults at

Three or nine Castor-2 solid rocket boosters were attached to increase thrust at lift-off. The Delta-P second stage used the TRW TR-201 engine. The TR-201

Atlas I by using engines with greater thrust and longer propellant tanks for both stages. The increased thrust, engine efficiency, and propellant capacity

types and classifications by region and historical era Swordsmanship Thrusting swords (Edgeless) Curved swords (Single-edge) Straight swords (Double-edge)

high, located at latitude 56.3 S and longitude 38.3 W. It was formed by a thrust fault, thought to have occurred due to the shrinkage of the planet's core

take-off for helping overloaded aircraft into the air by providing additional thrust in the form of small rockets. The term JATO is used interchangeably with

D (four strap-on boosters) Gross mass: 43.0 tons Empty mass: 3.400 tons Thrust (vac): 4 × 99,000 kgf = 396 Mgf (3.89 MN) Isp: 306 s (3,000 N·s/kg) Burn

may be a mix of different orogenic expressions and terranes, for example thrust sheets, uplifted blocks, fold mountains, and volcanic landforms resulting

demonstrator, the F-15 STOL/MTD carried out research for studying the effects of thrust vectoring and enhanced maneuverability. The aircraft used for the project

variant named "Long Tank Thrust Augmented Thor". The Long Tank Thor first stage was later adopted by NASA's Delta program for its "Thrust Augmented Improved

840 lbf) of dry thrust, 14.5 tonnes (142.2 kN, 31,970 lbf) of thrust in afterburner, and 15 tonnes (147.1 kN, 33,070 lbf) of thrust in "special" emergency

injector technology and design is also used on SpaceX Merlin engines. The thrust chamber was initially developed for the Apollo Lunar Module and was subsequently

and the AVD malfunction detection system, which would terminate engine thrust if the booster's operating parameters (engine performance, electrical power

burn for 130 seconds and produce an average thrust of 3,578.2 kilonewtons (804,400 lbf) and a peak thrust of 5,150 kilonewtons (1,160,000 lbf) each. The

total impulse). The S-IB first stage also increased the S-I baseline's thrust from 1,500,000 pounds-force (6,700,000 N) to 1,600,000 pounds-force (7,100

a mixture of gasoline and oil. These engines are favored for their high thrust-to-weight ratio of engine plus fuel; they use approximately 3.7 litres (1

intersection (a true ellipse) is known as a groin vault, down which the thrust of the vault is carried to the cross walls; if a series of two or more barrel

aircraft were produced and used for tests and demonstrations; one example had thrust-vectoring engines and was in turn redesignated the Su-37. A sole Su-35UB

the 1950s. The main objective of the project was to demonstrate vectored thrust horizontal and vertical takeoff, hover, transition to forward flight, and

The Rolls-Royce Thrust Measuring Rig (TMR) was a pioneering vertical take-off and landing (VTOL) aircraft developed by Rolls-Royce in the 1950s. It has

LR79-NA (model S-3D) rocket engine producing 667 kilonewtons (150,000 lbf) of thrust. It was armed with the 1.44 megatons of TNT (6.0 PJ) W49 nuclear warhead

instability while designing bigger thrust chambers. At that time, they solved the problem by using a cluster of smaller thrust chambers. The RD-170 engine featured

finer control of the second-stage burn, allowing operators to tune the thrust and even channel it through nozzles that helped orient the rocket for the

Camber thrust and camber force are terms used to describe the force generated perpendicular to the direction of travel of a rolling tire due to its camber

2013(2013-05-08) (aged 86) Virginia Water, Surrey, England Other names Turk Thrust Occupation(s) Filmmaker, actor, author Spouses Constance Smith ​ ​ (m. 1951;

instability while designing bigger thrust chambers. At that time, they solved the problem by using a cluster of smaller thrust chambers. The RD-170 engine featured

these situations, but low-energy transfers which take into account the thrust limitations of real engines, and take advantage of the gravity wells of

combustion Propellant Combination – LOX / LH2 Maximum thrust (Vacuum) – 73.55 kN Operating Thrust Range (as demonstrated during GSLV Mk2 D5 flight) – 73

forward of the wing was used as well as split ailerons and an advanced thrust vectoring nozzle for directional control. The X-36 was unstable in both

bucket, reverse thrust can also be achieved for faring backwards, quickly and without the need to change gear or adjust engine thrust. The reversing bucket

The Japanese Thrust, pp. 447–457 Johnston, The Silent 7th, p. 250 Wigmore, The Japanese Thrust, pp. 28–61 Wigmore, The Japanese Thrust, p. 382 Wigmore

Part of a series on Earthquakes Types Mainshock Foreshock Aftershock Blind thrust Doublet Interplate Intraplate Megathrust Remotely triggered Slow Submarine

jet thrust, the P.1127 had an innovative vectored thrust turbofan engine, the Pegasus. The Pegasus I was rated at 9,000 pounds (40 kN) of thrust and first

volcanic provinces. Recent research has unveiled the presence of extensive thrust faulting bounding the massif terrains. Since the 2010s, researchers have

specified thrust. To keep the engine thrust values consistent with previous documentation and software, NASA kept the originally specified thrust at 100%

swivel tangentially up to 7.0° from the neutral position, providing full thrust vector control. The rationale for this design is logistics: the diameter

engine developed a thrust of 315 kN for 116 seconds. The Topaze P-2.2 second stage had one P4 solid propellant engine that developed a thrust of 150 kN for

take hold on the top rope, thrusting the pelvis repeatedly against the opponent's midsection as if performing turnbuckle thrusts. Also known as vertical

1 was a significant evolution from Falcon 9 v1.0, with 60 percent more thrust and weight. Its maiden flight carried out a demonstration mission with the

projected thrust augmentation levels were highly optimistic, and that the aircraft would most likely be incapable of vertical flight on the thrust available

thrust of all five thrust chambers was 360,000 lbf (1,600 kN) for a standard Atlas D. Atlas E/F had 375,000 pounds of thrust. Total sea level thrust for

driver is a tool that delivers a strong, sudden rotational force and forward thrust. The force can be delivered either by striking with a hammer in the case

I Payload: 68 kg (150 lb) Maximum flight height: 225 km (140 mi) Launch thrust: 111 kN (25,000 lbf) Launch mass: 730 kg (1,610 lb) Diameter: 0.26 m (10 in)

of the theory of plate tectonics and before the internal architecture of thrust belts became well understood, the term was used to describe most mountain

use a high-thrust, low-efficiency launch vehicle to put their satellite into GTO, and then, after detaching the launch vehicle, use low-thrust, high-efficiency

The Lewis Overthrust is a geologic thrust fault structure of the Rocky Mountains found within the bordering national parks of Glacier in Montana, United

thoughts. A Research Thrust is the fundamental knowledge or basic research that investigators bring to the center. These thrusts feed into technologies

The Autobots are a fictional faction of sentient robots in the Transformers multimedia franchise. The Autobots are living robots from the planet Cybertron

mounted on a hydraulic actuated gimbal which enabled thrust vectoring to control pitch and yaw. Engine thrust and mixture ratio were controlled by cavitating

use a high-thrust, low-efficiency launch vehicle to put their satellite into GTO, and then, after detaching the launch vehicle, use low-thrust, high-efficiency

fold and thrust belt. The region is in the Basin and Range and three mountain ranges are in a parallel, northwest-by-southeast-trending thrust belt, with

knee. Khao thon [kʰàw tʰoːn] (Straight knee strike) – the boxer simply thrusts it forward but not upwards, unless he is holding an opponent's head down

operating the route crashed following an uncommanded deployment of the thrust reverser on the No. 1 engine during the climb phase, causing the aircraft

D (four strap-on boosters) Gross mass: 43,300 kg Empty mass: 3,710 kg Thrust (vac): 4 x 99,000 kgf (971 kN) = 3.88 MN Isp: 313 seconds (3.07 km/s) Burn

maneuver is much more useful for high-thrust rocket engines like liquid-propellant rockets, and less useful for low-thrust reaction engines such as ion drives

of the Rocketdyne MA-1 engines with conical thrust chambers that produced a mere 135,000 pounds of thrust, compared with the 360,000 pounds of the fully

plate and Eurasia. The thrust belt that marks this plate boundary zone is formed of a series of sub-parallel thrust faults. The thrust faults in this part

The Autobots are a fictional faction of sentient robots in the Transformers multimedia franchise. The Autobots are living robots from the planet Cybertron

density, A is the area of the wind turbine, and V is the wind speed. The thrust coefficient is another important dimensionless number in wind turbine aerodynamics

March 7, 1977. The first run was performed with a standing start at idle thrust and gradual acceleration and had an estimated top speed of about 180 mph

Thrust is the fourteenth studio album by American jazz-funk musician Herbie Hancock, released in September 1974 on Columbia Records. The album reached

manufacturer Bristol Engine Company, who were designing an innovative vectored thrust engine, British aviation conglomerate Hawker Aircraft developed their design

Mojave and northwest Sonoran Deserts. The region is named the Maria fold and thrust belt but here, southwest of the Date Creek's is the northwest of the region

at 04:30:55 PST. The epicenter of the moment magnitude 6.7 (Mw) blind thrust earthquake was beneath the San Fernando Valley. Lasting approximately 8

Jadar-Kopaonik Thrust Sheet is a NW-SE striking unit in the southern footwall of the Sava Zone and the northern hangingwall of the Drina-Ivanjica Thrust Sheet

initial production model, the revised airframe variant with new engines and thrust-vectoring control, and the aircraft-teaming capable twin-seat variant. Descending

the Puente Hills Thrust Fault System) is an active geological fault that is located in the Los Angeles Basin in California. The thrust fault was discovered

circular orbit to another with only one brief application of thrust. From a circular orbit, thrust applied in a direction opposite to the satellite's motion

approximately 42,000 lb. of thrust; an interstage; a forward stage SRM with 6,000 lb. of propellant generating approximately 18,000 lb. of thrust; and an equipment

provides an average thrust of 1,223 kilonewtons (275,000 lbf). The third stage then burns for 72 seconds, with an average thrust of 289 kilonewtons (65

suture zones or dipping thrust faults. These thrust faults carry relatively thin slices of rock (which are called nappes or thrust sheets, and differ from

in modern theatres. A proscenium stage is structurally different from a thrust stage or an arena stage, as explained below. In later Hellenistic Greek

The adverse consequences of this simplicity were a significantly lower thrust-to-weight ratio and a 10% lower specific impulse compared to the SSME. The

Delta M. Three Castor-2 solid rocket boosters were attached to increase thrust at lift-off. A Delta E was used as the second stage. If an increased payload

arc-shaped ranges, and two intermountain valleys in the Maria fold and thrust belt, a region in western Arizona and southeast Southern California, with

pioneered modern methods such as two-axis control (gyroscopes and steerable thrust) to allow rockets to control their flight effectively. Although his work

featured the AVD malfunction detection system which would terminate engine thrust in-flight if it detected a deviation from the booster's normal performance

decreased atmospheric pressure at higher altitudes. This staging allows the thrust of the remaining stages to more easily accelerate the rocket to its final

propellant 40 tons, the second will have 30 tons of thrust engine and the latter will be 7.5 tons of thrust, with the same mixture "Kerolox". It can place

(10,200,000 lbf) of thrust, the most powerful rocket stage flown to date.: 199  This exceeded the 33,700 kN (7,600,000 lbf) thrust of the Saturn V, and

The burpee, a squat thrust with an additional stand between repetitions, is a full body exercise used in strength training. The movement itself is primarily

5 in) Propellant mass 37,700 kg (83,100 lb) Powered by 1 YF-25 Maximum thrust 740.4 kN (166,400 lbf) Specific impulse 2,556.2 m/s (8,386 ft/s) Burn time

arc-shaped ranges, and two intermountain range valleys in the Maria fold and thrust belt, a region in western-central Arizona and southeast Southern California

engine, with removal of one thrust chamber and a rerouting of the plumbing to allow the engine to fit within the smaller Thor thrust section. Engine component

shaft or any other two mating surfaces (e.g., a slide plate). Thrust bearing: A thrust bearing provides a bearing surface for forces acting axial to the

cycle and utilized a regeneratively cooled combustion chamber. For each thrust chamber assembly, a single high-speed turbine drove the lower-speed centrifugal

has been moved from its original site of formation, usually by low angle thrust faulting. The term is derived from Greek: allo, meaning other, and chthon

(09:00:22 local time) with an epicenter in the Tien Shan mountains. The thrust earthquake measured 7.7 on the moment magnitude scale (Mw ) and had a depth

X-31 is an experimental jet aircraft designed to test fighter thrust vectoring technology. It was designed and built by Rockwell and Messerschmitt-Bölkow-Blohm

rockets. Nine Castor-4A solid rocket boosters were attached to increase thrust at lift-off, replacing the less powerful Castor-4 boosters used on the 3000

gas-generator combustion cycle. It has a four combustion chambers that provide thrust vector control by gimbaling each nozzle in a single axis ±55°. It is used

load. Thrust bearings come in several varieties. Thrust ball bearings, composed of bearing balls supported in a ring, can be used in low-thrust applications

Formation Autonomy Spacecraft with Thrust, Relnav, Attitude and Crosslink (or FASTRAC) is a pair of nanosatellites (respectively named Sara-Lily and Emma)

available for AESA radar. The serial production aircraft does not have thrust vectoring control as previously planned. There were references in the late

sliding). Mechanically weak layers in strata allow the development of stepped thrusts (either over- or underthrusts), which originate at subduction zones and

and likely would have fixed axisymmetric engine nozzles as opposed to the thrust vectoring nozzles on the F-22. Though not designed for supercruise, the

altitude control while in the atmosphere. The first stage does not have a thrust vector control (TVC) system. Pegasus was designed by a team led by Antonio

stage – SR-118 Maximum thrust 2,200 kN (490,000 lbf) Burn time 83 seconds Propellant HTPB Second stage – SR-119 Maximum thrust 1,365 kN (307,000 lbf)

other minor problem was evident: At T+179 seconds, Titan thrust assembly #2 experienced a 2% thrust decay. This was accompanied by a small drop in turbopump

performance would require a lower-stage booster with a thrust of about 1.5 million pound-force (6.7 MN) thrust at takeoff. As it happened, the Air Force had recently

with spiral rollers Ball radial-thrust single-row Roller tapered Ball thrust, ball thrust-radial Roller thrust or thrust-radial The fifth and sixth digit

Mercury. Discovered by the Mariner 10 spacecraft in 1974, it was formed by a thrust fault, thought to have occurred due to the shrinkage of the planet's core

capable of throttling down to 30% of nominal thrust; the design also allows for a short-duration enhanced thrust (up to 105% of nominal level) in emergency

combustion chamber was regeneratively cooled. The engine was gimbaled to supply thrust vectoring. Also, the exhaust gases of the turbine were ducted to dual auxiliary

engine failure. When aircraft are certified according to ETOPS standards, thrust is not an issue, as one of the engines is more than powerful enough to keep

staged combustion cycle. It has a four combustion chambers that provide thrust vector control by gimbaling each of the nozzles in a single axis ±33°. It

Sukhoi Su-27, the first aircraft to publicly display thrust vectoring in pitch. Combined with a thrust-to-weight ratio above unity, this enabled it to maintain

The Maria fold and thrust belt (MFTB) is a portion of the North American Cordillera orogen in which geological structures accommodate roughly north–south

however remained within normal levels until missile destruction. A minor thrust section fire was evident from T+9 seconds, caused by placement of the lube

the RD-58M (manufacturer designation 11D58M), which has slightly reduced thrust, but increased isp. An even newer version is under development and is known

47-degree inclination. At liftoff, the ASLV generated 909.9 kN (204,500 lbf) of thrust. It was a 41,000-kilogram (90,000 lb) rocket, measuring 23.5 metres (77 ft)

Francis Matthews (2 September 1927 – 14 June 2014) was an English actor, best known for playing Paul Temple in the BBC television series of the same name

expander bleed cycle engine to generate large thrust, so the development of the LE-9 engine with a thrust of 1,471 kN (331,000 lbf) is the most challenging

slip, albeit modulated by end effects. Equations exist for calculating the thrust of a motor. Unlike a circular induction motor, a linear induction motor

stage (Demonstration Flight/Enhanced) – SRB-A3 Powered by 1 solid Maximum thrust 2,271 kN (511,000 lbf) Specific impulse 284 s (2.79 km/s) Burn time 116

These include head and neck maneuvers to optimize ventilation, abdominal thrusts, and back blows. Advanced techniques require specialized medical training

biomechanics (see section below), the term high velocity low amplitude (HVLA) thrust is often used interchangeably with manipulation.[citation needed] Manipulation

The Maria fold and thrust belt (MFTB) is a portion of the North American Cordillera orogen in which geological structures accommodate roughly north–south

expander bleed cycle engine to generate large thrust, so the development of the LE-9 engine with a thrust of 1,471 kN (331,000 lbf) is the most challenging

The engine has been designed to produce 670 kilonewtons (150,000 lbf) of thrust at sea level. The engine passed its first power pack test including the

upgraded version of the YF-75D engines (known as the YF-75H) with increased thrust to 10 tonnes each through measures such as increased turbopump speeds. The

highest target thrust among all commercial rocket engines in China. The engine features deep throttling for reusability, re-ignition, thrust vectoring, and

exchanger (FOHE) of each engine. This restricted fuel flow to the engines when thrust was demanded during the final approach to Heathrow. The AAIB identified

its first 300 seconds test fire in November 2007. A high efficiency/high thrust environmentally-friendly rocket engine was always an objective within Programme

and bonus tracks from single releases. Def Leppard began their Downstage Thrust Tour, on 27 June, which took them across the US and into Canada. On 25 April

copies in the first six months. This was followed by the releases of Brain Thrust Mastery in 2008, Barbara in 2010, TV en Français in 2014, Helter Seltzer

“Pusher configuration” describes the specific (propeller or ducted fan) thrust device attached to a craft, either aerostats (airship) or aerodynes (aircraft

aircraft with this push-pull, or "centerline thrust," configuration are restricted to flying centerline-thrust aircraft; pilots who obtain a multi-engine

launched from Vandenberg Air Force Base in California. The Falcon 9 Full Thrust and Falcon Heavy variants followed in 2015 and 2018. Falcon Heavy launches

recorded the left thrust lever being retarded to the rear-most position, activating the thrust reverser on the left engine, while the right thrust lever (controlling

total thrust. OSO 4 is an example of a Delta C launch.[citation needed] Delta D, also known as Thrust Augmented Delta, was a Delta C with the Thrust Augmented

operated by SES It was launched from Cape Canaveral SLC-40 by a Falcon 9 Full Thrust launch vehicle on 4 March 2016. SES-9 is a large communications satellite

Calif. First stage: Length: 70 ft (21 m) Diameter: 10 feet (3.05 m) Engine thrust: 474,000 lbf (2,110 kN) vacuum Weight: 258,000 pounds (117,000 kg) Fueled

600 lbf) of thrust and has a specific impulse of 311 s (3.05 km/s), while the vacuum optimized-version produces 25.8 kN (5,800 lbf) of thrust and has a

cycle and with a thrust of 44.15 kilonewtons (9,930 lbf). It had four hinge mounted nozzles that gimbaled each on one axis to supply thrust vector control

000 pounds-force (4 kN) thrust, but was converted in Spring 2009 to be powered by one engine of 750 pounds-force (3 kN) thrust. By October 2009, the regeneratively

Aerojet XASR-1 2,600 lbf (12 kN) thrust air-pressurized engine. Aerojet's XASR-1 was developed from the 1,500 lbf (7 kN) thrust WAC-1 engine of the WAC Corporal

specifying the thrust of the nine Archimedes engines used on the first stage as 5,960 kN (1,340,000 lbf) at sea level and a maximum thrust of 7,530 kN (1

engines generating up to 37,000 kilograms-force (360 kN; 82,000 lbf) of thrust. The first stage also utilize a set of four vernier engines sharing a single

the Bill Williams River northern bank — is the Maria fold and thrust belt. The thrust belt is a geographic and geologic region at the convergence of

allow for high lift at low speeds, large control surface deflections, or thrust vectoring. The Aviat Eagle, after stalling, is able to gain some degree

generation fighter aircraft are viable. The aircraft features 3-D thrust vectoring capability. Thrust is controlled in the ATD-X by three paddles on each engine

afterburning turbofan engines, 93.1 kN (20,900 lbf) thrust each engines with 2-dimensional and 3-dimensional thrust-vectoring nozzles planned for testing. dry

is powered by a YF-100 engine, which generates 1,340 kN (300,000 lbf) of thrust from burning kerosene and LOX as rocket fuel and oxidiser. This was the

afterburning turbofan engines, 93.1 kN (20,900 lbf) thrust each engines with 2-dimensional and 3-dimensional thrust-vectoring nozzles planned for testing. dry

deformation in plate tectonics at a convergent boundary which occurs with shallow thrust faults that only involves cover rocks (typically sedimentary rocks), and

increasingly used in recent years to advance maneuverability via the use of thrust vectoring engine nozzles. Russian emphasis on close-range slow-speed supermaneuverability

between the years 1902 to 1930. Kingsbury is most famous for his hydrodynamic thrust bearing which uses a thin film of oil to support weights of up to 220 tons

lithosphere allows subsidence near the thrust, narrowing of basin, forebulge toward thrust. During times of thrusting, the lithosphere is stiff and the forebulge

Aérocentre NC.130 1939 – High-altitude flight Aérospatiale Ludion 1967 – Thrust vectored rocket VTOL Arsenal-Delanne 10 – Tandem wing Arsenal VG 70 – High

decides to go around, the pilot applies full thrust or a predetermined TOGA (Takeoff and Go Around) thrust to the engine(s), adopts an appropriate climb

less sea level thrust (78,000 pounds-force (350 kN)) than the Launch Escape System rocket (150,000 pounds-force (667 kN) sea level thrust) mounted atop

Gimbaled thrust is the system of thrust vectoring used in most rockets, including the Space Shuttle, the Saturn V lunar rockets, and the Falcon 9. In a

resulting up-thrust is known as Archimedes' principle, which states: "when an object is wholly or partially immersed in a liquid, the up-thrust it receives

single set of helical teeth will produce a thrust parallel to the axle of the gear (known as axial thrust) due to the angular nature of the teeth. By

the Bill Williams River northern bank — is the Maria fold and thrust belt. The thrust belt is a geographic and geologic region at the convergence of

the thrust in kilograms-force on the mass of an engine or a rocket in kilograms conveniently gives the thrust to weight ratio, dividing the thrust on propellant

1980. Two of these engines were used in the Titan III GTO Transtage, with thrust uprated from 7,800 lbf (35 kN) to 8,000 lbf (36 kN), and with a higher specific

Engine Company's choice to invest in the creation of the Pegasus vectored-thrust engine. Testing began in July 1960 and by the end of the year the aircraft

RS-27 used on the 6000-series Delta II produced 915 kN (206,000 lbf) of thrust, while the upgraded RS-27A used by the 7000-series produced 1,054 kN (237

structural geology the term was first used to describe the thrust-bounded imbricates found within a thrust duplex. In later literature it has become a general

faulting on a thrust system. In such a system the rock mass (hanging wall block) that has been transported by movement along the thrust is called a nappe

increased via a titanium heat exchanger on the ablative/niobium boundary. Thrust vector control is provided by electro-mechanical actuators on the engine

The RD-107 has an additional two vernier combustion chambers that can thrust vector in a single plane to supply attitude control. The RD-108 has four

nitrogen tetroxide as oxidant, producing 37 tons (363 kN; 82,500 lbf) of thrust. The second stage utilizes a pair of smaller engines (originally the Vernier

wedge is similar to that found in a thin-skinned foreland thrust belt. A series of thrusts verging towards the trench are formed with the youngest most

The SRMU participates in vehicle control using a hydraulically driven thrust-vectoring nozzle, which can move up to 6 degrees. The hydraulic system features

vacuum of thrust. Its specific impulse is 300 s (2.9 km/s) at sea level and 335 s (3.29 km/s) in vacuum. Each module has its own single axis thrust vector

causes mayhem. With a re-think and given the name of the "Hammerhead Eagle i-Thrust", the presenters take it to the MIRA Proving Ground and try pass the EU-required

capsule, previously flown on CRS-6. The first stage of the Falcon 9 Full Thrust rocket was the previously flown, "flight-proven" core from CRS-11. The first

The Zagros fold and thrust belt (Zagros FTB) is an approximately 1,800-kilometre (1,100 mi) long zone of deformed crustal rocks, formed in the foreland

engineers wondered whether the Ryan/U.S. Navy FR-1 Fireball, which had a thrust-to-weight ratio of 1 at low fuel quantities, would take off vertically.

powered by Welkin engines. Seven Welkin engines producing 280 tonnes of thrust will be powering the first stage, while the second stage will be powered

A jet engine performs by converting fuel into thrust. How well it performs is an indication of what proportion of its fuel goes to waste. It transfers

crew increased the thrust of both engines and retracted the flaps and landing gear. The right engine began delivering forward thrust but the left engine

technology. While the engine is capable of 73,000 newtons (16,400 lbf) of thrust, during use for DragonFly testing, the engines were throttled to 68,170

January 2016, and the Falcon 9 Full Thrust (through Block 4) 36 times from December 2015, to June 2018. The latest Full Thrust variant, Block 5, was introduced

Powered by 1 Solid Maximum thrust 935 kilonewtons (210,000 lbf) Propellant Solid Second stage – SR19 Powered by 1 Solid Maximum thrust 268 kilonewtons (60,000 lbf)

staged combustion cycle. It has a single combustion chamber that provides thrust vector control by gimbaling of the nozzle in two axis by +/- 6°. It is being

descending to the runway. This speed reduction is accomplished by reducing thrust and/or inducing a greater amount of drag using flaps, landing gear or speed

staged combustion cycle. It has a single combustion chamber that provides thrust vector control by gimbaling of the nozzle in two axis by +/- 6°. It is being

faulting on a thrust system. In such a system the rock mass (hanging wall block) that has been transported by movement along the thrust is called a nappe

set of sandstone peaks and walls that were formed by thrust faults including the Keystone Thrust. The walls are up to 3,000 feet (910 m) high, making

rocket was destroyed by the range safety officer after the failure of its thrust vectoring system resulted in a loss of control. The launch was the first

The Mount Diablo Thrust Fault, also known as the Mount Diablo Blind Thrust, is a thrust fault in the vicinity of Mount Diablo in Contra Costa County, California

mountain ranges on the north of an insular region called the Maria fold and thrust belt, containing mountain ranges, valleys, and plains. The Rawhide Mountains

were no reasonably priced launch vehicles with the payload capability and thrust versatility that could meet the requirements of the planned tests, a contract

thrust faulting along a fault located in the back-arc region between the Sunda and Banda island arcs. The Flores Thrust represents a back-arc thrust fault

controlled. The thrust in fact varies, for two reasons. Firstly, as the pressure in the oxidizer tank decreases, the flow rate reduces, reducing thrust. Secondly

local sonic shock waves where the airflow becomes transonic at high speeds. Thrust gates, or gaps, in the trailing edge flaps may be required to minimise interference

700 lb) Powerplant: 2 × Tumansky R-27-300 Vectored thrust axial flow turbojets, 52 kN (12,000 lbf) thrust each Performance Maximum speed: 900 km/h (560 mph

to provide the expected full thrust in all of its three burns due to a leak above the narrow throat portion of the thrust chamber, however the stage had

The Northridge Blind Thrust Fault (also known as the Pico Thrust Fault) is a thrust fault that is located in the San Fernando Valley area of Los Angeles

Thrust is a 1986 video game programmed by Jeremy C. Smith (who later co-authored Exile) for the BBC Micro and published by Superior Software. The player's

Maximum thrust 440 kilonewtons (99,000 lbf) Burn time 44 seconds Propellant Solid Second stage – Castor 1A Powered by 1 solid Maximum thrust 286 kilonewtons

strongly that unstable engine thrust resulted. The result of this was to trip the first stage pressure switch and terminate thrust early. The second stage then

21 kilonewtons (4,700 lbf) of more thrust. It has a fixed nozzle and relies on the RD-0236 vernier engine for thrust vectoring. While the engine has been

called the Shakespeare Memorial Theatre) is a Grade II* listed 1,040+ seat thrust stage theatre owned by the Royal Shakespeare Company dedicated to the English

Comic novels are often defined by the author's literary choice to make the thrust of the work—in its narration or plot—funny or satirical in orientation,

first stage booster uses four KRE-075 SL engines generating 266.4 tons of thrust with a specific impulse of 289.1 seconds. The second stage booster uses

southern part. It is delineated by the Himalayan Frontal Thrust (HFT) and Main Boundary Thrust (MBT) in south and north respectively. The youngest sediments

the plane's autothrottle; the thrust lever for the left engine reduced thrust as the aircraft climbed, while the thrust lever for the right engine remained

and Switzerland will manufacture the engine. The M10 minimum thrust requirements are a thrust of 98 kN (22,000 lbf) with a propellant mixture ratio of 3

assumes that the Oberth effect is being used—this is possible with high thrust chemical propulsion but not with current (as of 2018) electrical propulsion

engine, both in size and thrust output, being in the 89 kN (20,000 lbf) and the more recent models the 130 kN (30,000 lbf) thrust class. The motor is capable

was named after a Confederate General James Longstreet. Operation Desert Thrust October 2003 October 2003 throughout Iraq Counterinsurgency: Was the name

(85% hydrogen peroxide + 15% water). While the first two stages featured thrust vectoring to provide attitude control, the third stage did not have an attitude

April 25, 1997 Boosters – MA-5 No. boosters 1 Powered by 2 LR-89-7 Maximum thrust 1,901.6 kN (427,500 lbf) Specific impulse 293.4 s (2.877 km/s) Burn time

and near the Aleutian Island arc and depending on the location, there is thrust faulting, strike-slip faulting, and normal faulting. These result in an

splitting the casings open to release the pressure inside and terminate thrust. The ISDS would end up being used a few times over the Titan's career. Another

The failure was traced to a leak in a LOX line that caused a fire in the thrust section of the booster. Estimated repair costs were about 45 million rubles

crewed spacecraft. Very little advanced research had been done in variable-thrust rocket engines up to that point. Rocketdyne proposed a pressure-fed engine

orbit when one second-stage motor failed to ignite, causing imbalanced thrust that sent the payload into the Atlantic Ocean. In mid-1960, with only two

while the RS-56-OSA was designed for use as a sustainer and produced lower thrust but at a higher specific impulse. "Atlas IIA(S) Data Sheet". Space Launch

ICBM hardware such as retrorockets. Although the main engines had greater thrust, the verniers were detuned slightly in the interest of improved ISP (vacuum

Mercury. Discovered by the Mariner 10 spacecraft in 1974, it was formed by a thrust fault, thought to have occurred due to the shrinkage of the planet's core

The failure was traced to a leak in a LOX line that caused a fire in the thrust section of the booster. Estimated repair costs were about 45 million rubles

well-designed low-drag radiators (notably the P-51 Mustang) derive thrust from it. The thrust was significant enough to offset the drag of the duct the radiator

orbit when one second-stage motor failed to ignite, causing imbalanced thrust that sent the payload into the Atlantic Ocean. In mid-1960, with only two

Maximum thrust 440 kilonewtons (99,000 lbf) Burn time 44 seconds Propellant Solid Second stage – Castor 1A Powered by 1 solid Maximum thrust 286 kilonewtons

Last flight 1961-11-01 First stage – Algol 1B Powered by 1 solid Maximum thrust 471 kilonewtons (106,000 lbf) Specific impulse 236 sec Burn time 40 seconds

Mercury. Discovered by the Mariner 10 spacecraft in 1974, it was formed by a thrust fault, thought to have occurred due to the shrinkage of the planet's core

of 6,500 lbf (29 kN) thrust. These were quickly replaced by Armstrong Siddeley Sapphire ASSa.6 engines of 7,500 lbf (33 kN) thrust. VX770 later became

delta wings, a single vertical tail, and twin engines with thrust vectoring nozzles and thrust reversers. Around this time, however, the SPO would begin

This engine was vacuum optimized and ran the gas-generator cycle. The thrust chamber used fuel for regenerative cooling, with separate ablative skirt

74 tons (725 kN; 163,000 lbf) of thrust and a Safir type 1.25m diameter liquid-fuel (UDMH /N2O4) engine with a thrust of 3.5 tons (35 kN; 7,800 lbf) as

a trade secret. The kick stage rocket produces 120 newtons (27 lbf) of thrust, and has a specific impulse of approximately 320 seconds. It was first used

First stage Propellant mass 8.6 t (19,000 lb) Powered by 1 solid Maximum thrust 450 kN (100,000 lbf) Specific impulse 253 seconds (2.48 km/s) Burn time

sacrifice,[citation needed] or refer to a single edged cutting or "cut and thrust" sword with a similarly shaped blade. The term derives from the Greek word

into the injector head and destroy it, causing complete loss of engine thrust. After the failure of Vanguard TV-3, the backup vehicle, Vanguard TV-3BU

exposed in today's Appalachian Mountains reveal elongate belts of folded and thrust faulted marine sedimentary rocks, volcanic rocks, and slivers of ancient

460 lb) Propellant mass 143,692 kg (316,787 lb) Powered by 4 YF-21B Maximum thrust 2,961.6 kN (665,800 lbf) Specific impulse 2,556.2 m/s (260.66 s) Burn time

plans to create jet engines in the 1,000 to 3,500 lbf (4.4 to 15.6 kN) thrust class, suitable for the business aviation industry. GE Honda HF120 "About

non-catapult-assisted fixed-wing short takeoffs are accomplished with the use of thrust vectoring, which may also be used in conjunction with a runway "ski-jump"

February 1987 Boosters – Castor 2 No. boosters 9 Powered by 1 TX-354-3 Maximum thrust 258.9 kilonewtons (58,200 lbf) Specific impulse 262 sec Burn time 37 seconds

Jupiter Thrust: 600.1 kN (134908 lbf). Specific impulse: 282 s. Burn time: 247 s. Rocketdyne S-3: First flight: 1958 Vehicles: Juno II, Saturn A-2 Thrust: 667

drag created by the spoilers directly assists the braking effect. Reverse thrust is also used to help slow the aircraft after landing. Virtually all jet-powered

prototype was tested at 60% and 100% (25 tonnes-force (250 kN; 25 LTf; 28 STf)) thrust levels in December 2021. It will be used on the third stage of the Long

Kingston upon Thames in London, England. The theatre seats 822 around a wide, thrust stage. It officially opened on 16 January, 2008 with the play Uncle Vanya

Posed with the requirement to produce a rocket with substantially greater thrust, the design team considered various approaches to achieve this.: 179  One

gyroscopic force in lieu of a guidance system that would have required thrust vectoring, vernier thrusters, or a reaction control system. The booster

ring-shaped airfoil is positioned so this lift effect is forward. This thrust does not fully counter the drag of the cowl but greatly mitigates it. The

The Ouachita orogeny was a mountain-building event that resulted in the folding and faulting of strata currently exposed in the Ouachita Mountains. The

RD-107-8D74 Maximum thrust 970 kilonewtons (220,000 lbf) Burn time 120 seconds Propellant RP-1/LOX First stage Powered by 1 RD-108-8D75 Maximum thrust 912 kilonewtons

The Rocketdyne H-1 was a 205,000 lbf (910 kN) thrust liquid-propellant rocket engine burning LOX and RP-1. The H-1 was developed for use in the S-I and

A klippe (German for cliff or crag) is a geological feature of thrust fault terrains. The klippe is the remnant portion of a nappe after erosion has removed

ring-shaped airfoil is positioned so this lift effect is forward. This thrust does not fully counter the drag of the cowl but greatly mitigates it. The

States, at 7:42 a.m. PDT on October 1. The moderate magnitude 5.9 blind thrust earthquake was centered several miles north of Whittier in the town of Rosemead

the top to create a through bridge. Because no moments are transferred, thrust (as from an arch bridge) cannot be accommodated, leading to innovative designs

arrangement in the thrusters used during hover, greatly increasing their thrust. The release of NATO Basic Military Requirement 3 for a VTOL strike-fighter

productions, ceremonies and lectures. Diamond Theater - a small 309-seat 3/4 thrust theater with steeply raked stadium seating suited for theatrical and small

UR-700 and UR-900 rocket families, as well as on the N1. It has the highest thrust among single-chamber engines of the USSR, 640 metric tons at the surface

(satellite) Boosters No. boosters 4 Powered by 1 RD-107 Maximum thrust 995.4 kN (223,800 lbf) Total thrust 3,981.6 kN (895,100 lbf) Specific impulse 257 seconds

The Delta D, Thrust Augmented Delta or Thor-Delta D was an American expendable launch system used to launch two communications satellites in 1964 and 1965

Height 15.1 m (50 ft) Diameter 2.5 m (8 ft 2 in) Maximum thrust 2,260 kN (510,000 lbf) Total thrust 4,520–9,040 kN (1,020,000–2,030,000 lbf) Specific impulse

The engine has been designed to produce 2.4 meganewtons (550,000 lbf) of thrust at sea level. It was initially planned for the engine to be used exclusively

goal of enabling crewed lunar missions by the USSR. The KVD-1 produces a thrust of 7.5 tonnes. KVD-1 was originated from the RD-56 engine which were intended

one for liquid hydrogen, and a Vulcain 2 engine at the base with a vacuum thrust of 1,390 kN (310,000 lbf). The H173 EPC weighed about 189 t (417,000 lb)

currently in development. It has been designed to reach around 500 tonnes of thrust and it will power the super heavy Long March 9 rocket. Chinese researchers

four chambers and four nozzles) for thrust vector control. The RD-0110R engines add 230.5 kN (51,800 lbf) thrust and heats the pressurization gases. The

flight, was replaced by a single Russian RD-180 engine, boasting higher thrust and efficiency than previous engines. Unlike Atlas II and the later Atlas V

cannot have their engines shut down, but splitting them open terminates thrust even though the propellant will continue to burn, as the explosive charges

force. Other perturbing forces include: Earth's albedo, navigation antenna thrust, and thermal effects related to heat re-radiation. The MEO region includes

included adding extra strap-on solid motors, higher-thrust main engines, lighter materials, higher-thrust second stages, more (up to eight) strap-on CBCs

left-side engines to continue generating forward thrust, while the right-side engines generated reverse thrust. The plane immediately began to veer to the

which culminated in the development of the Moine Thrust Belt, Ben Hope Thrust and Naver-Sgurr Beag Thrust (435–420 Ma) and led to igneous intrusion in Galloway

each Propellant mass 66,000 kg (146,000 lb) each Maximum thrust 2,305 kN (518,000 lbf) Total thrust 9,220 kN (2,070,000 lbf) Specific impulse 283.6 s (2.781 km/s)

stability without the acoustic resonance chambers that the SSME required. Thrust (vacuum): 1.8639 MN (190 tons), (sea-level): 1.5171 MN Specific impulse

several delays, SES-10 was launched on 30 March 2017 aboard a Falcon 9 Full Thrust. The launch marked the first time in aerospace history that an orbital-class

219 kg (198,899 lb) LOX: 236,567 kg (521,541 lb) Powered by RD-171 Maximum thrust Sea Level: 7,257 kN (1,631,000 lbf) Vacuum: 7,908 kN (1,778,000 lbf) Specific

boundary between the Chilean Central Valley and the Andes. As an active thrust fault it constitutes a seismic hazard zone for the densely populated Santiago

overall structure, the Flores Back Arc Thrust Fault. However, according to scientists, it happened on a different thrust fault as there are many individual

launch and the effect of the SRMU thrust force on the Titan IV vehicle were modeled. To evaluate the magnitude of the thrust force, the SRMU was connected

thrusters are used when a heavy spacecraft requires a wide range of different thrust levels for attitude or velocity control, as for maneuvering during docking