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Pelvic thrust (750 words) [view diff] exact match in snippet view article find links to article

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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)

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.

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

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

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

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)

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

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

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

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

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)

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

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

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

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)

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

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

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

118 seconds Engines: Soyuz and Soyuz-U models RD-107 Thrust 813 kN (183 klbf) at liftoff Thrust 991 kN (223 klbf) in vacuum Specific impulse 245 seconds

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

upgraded engine thrust on the URM-1 stages. The thrust up the URM-1 boosters would be 10% higher during the first 40 seconds to allow good thrust/weight ratio

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

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)

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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 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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

1000-series. 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

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

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

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

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

(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

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

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

Tongue thrust, also called reverse swallow or immature swallow, is a pseudo-pathological name for an adaptive lip seal mechanism, whereby normal nasal

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

(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

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

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

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

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

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

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

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

was an expendable, high efficiency, medium-sized motor with sufficient thrust for use on the H-II. The fuel turbopump had an issue using the originally

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

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

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

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

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

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

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

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)

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

propellant fuel with a loaded mass of 10,705 kg, and produces 470.93 kN of thrust. The motor has a specific Impulse of 236 seconds in a vacuum environment

A blind thrust earthquake occurs along a thrust fault that does not show signs on the Earth's surface, hence the designation "blind". Such faults, being

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

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

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

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

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

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)

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

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

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

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

was an expendable, high efficiency, medium-sized motor with sufficient thrust for use on the H-II. The fuel turbopump had an issue using the originally

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

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

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

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

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

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

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

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

Powered by 1 J57-8 Maximum thrust 71.14 kilonewtons (15,990 lbf) Propellant JP-4/Air First stage Powered by 2 HOTROC Maximum thrust 63.2 kilonewtons (14,200 lbf)

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

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

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

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

pressures and temperatures along the engine, thrust and propellant mass flow rates at different thrust profiles. Additionally, the engine served to test

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

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

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

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

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

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

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

(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

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

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

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

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

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

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

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

Deformation has induced large-scale intraplate shear and thrust faulting far from the plate boundary. Thrusting along the Tien Shan mountains has shortened the

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

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

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

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

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

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

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)

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

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

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

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

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

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

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

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.

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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 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

to the Moon, produce high thrust with low specific impulse, whereas electric ion engines produce a small amount of thrust very efficiently. Orion, by

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

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

Fold and Thrust Belt extends from southern California near the Mexican border to Canada. Basin and Range faults cut the older Sevier thrust faults. The

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

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

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 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

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

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 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

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"

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

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

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

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

vehicles. Within the mount, each engine can gimbal individually to enable thrust vectoring control. As with its predecessor YF-75, the YF-75D can adjust

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

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

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

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

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

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

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

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

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

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

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

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

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

operation was aimed against the Rur River, as a staging point for a subsequent thrust over the river to the Rhine into Germany. It was conducted by the First

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

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

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"

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

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

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

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

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

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

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

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

gases are distributed by an electrically driven system that can control the thrust among the nozzles. Between 1958 and 1960, Valentin Glushko's OKB 456 developed

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

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

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

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

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

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

gases are distributed by an electrically driven system that can control the thrust among the nozzles. Between 1958 and 1960, Valentin Glushko's OKB 456 developed

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

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

(UTC-2), the starboard engine of the Fokker 100 operating the route reversed thrust while the aircraft was climbing away from the runway at Congonhas. The aircraft

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

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

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

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

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

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

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

fuel and ignite the mixture. The resulting expansion of gases produces thrust. The compressors generally can ingest air only at subsonic speeds. To operate

with the neighbouring Northern Highland Terrane is formed by the Moine Thrust Belt. The basement is formed by Archaean and Paleoproterozoic gneisses of

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

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

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

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

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

carbon-fiber composite nozzle. Merlin 1A produced 340 kilonewtons (76,000 lbf) of thrust and was used to power the first stage of the first two Falcon 1 flights

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

the southernmost island province of Hainan. In July 2012, a new 1200 kN thrust LOX/kerosene engine to be used on the Long March 5 boosters was test-fired

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)

(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

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

intensity of IX (Violent). This thrust event was instrumentally recorded and occurred along the Main Central Thrust in the Uttarkashi and Gharwal regions

Maximum thrust 970.86 kN Total thrust 3883.4 kN Burn time 118 seconds Propellant RP-1/LOX First stage Powered by 1 RD-108-8D75-1959 Maximum thrust 912 kN

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

GEM-63XL solid rocket boosters falling off which led to reduced, asymmetrical thrust. The Vulcan Centaur re-uses many technologies from ULA's Atlas V and Delta

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

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

mounted directly to the aft portion of the fuselage. The thrust from the two 920-pound (4.09 kN) thrust engines caused turbulent airflow over the standard elevators

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)