rocket engine oor Masedonies
rocket engine
en
A reaction engine that obtains thrust by jet propulsion which forms its jet exclusively from propellant.
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ракетен мотор
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reaction engine
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Wernher von Braun was the lead rocket engineer for Nazi Germany's World War II V-2 rocket project.
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Some high-altitude rocket engines use ablative cooling, where the walls gradually erode in a controlled fashion.
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The temperature stability of niobium-containing superalloys is important for its use in jet and rocket engines.
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1950’s: Rocket engineer Wernher von Braun describes a wheel-shaped station orbiting 1,075 miles [1,730 km] above earth.
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A rocket-powered aircraft or rocket plane is an aircraft that uses a rocket engine for propulsion, sometimes in addition to airbreathing jet engines.
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Cooling systems usually employ air (air-cooled) or liquid (usually water) cooling, while some very hot engines using radiative cooling (especially some rocket engines).
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The carrier aircraft, run by experienced NASA pilots, will reach an altitude of # km before separating from the plane with rocket engines and continue to fly at a speed of # km/h
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The 11D33 engine was the world's first staged-combustion-cycle rocket engine, and also the first use of an ullage engine to allow a liquid-fuel rocket engine to start in space.
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Iridium is a good catalyst for the decomposition of hydrazine (into hot nitrogen and ammonia), and this is used in practice in low-thrust rocket engines; there are more details in the monopropellant rocket article.
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A rocket is propelled forward by a thrust force equal in magnitude, but opposite in direction, to the time-rate of momentum change of the exhaust gas accelerated from the combustion chamber through the rocket engine nozzle.
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This can be done in several ways including by the spinning blades of a propeller, or a rotating fan pushing air out from the back of a jet engine, or by ejecting hot gases from a rocket engine.
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Weightlessness is in contrast with current human experiences in which a non-uniform force is acting, such as: standing on the ground, sitting in a chair on the ground, etc., where gravity is countered by the support force of the ground, flying in a plane, where a support force is transmitted from the lift the wings provide (special trajectories which form an exception are described below), during atmospheric reentry, or during the use of a parachute, when atmospheric drag decelerates a vehicle, during an orbital maneuver in a spacecraft, or during the launch phase, when rocket engines provide thrust.
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Glushko designed many of the engines used on the early Soviet rockets, but was constantly at odds with Korolev.
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Phase 4: Rocket keeps firing its engines in the opposite direction of K, during the same time Ta according to clock K, until K' regains the same speed V with respect to K, but now towards K (with velocity −V).
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Some engines such as solid rockets have oxidisers already within the combustion chamber but in most cases for combustion to occur, a continuous supply of oxidiser must be supplied to the combustion chamber.
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Phase 5: Rocket keeps coasting towards K at speed V during the same time Tc according to clock K. Phase 6: Rocket again fires its engines in the direction of K, so it decelerates with a constant proper acceleration a during a time Ta, still according to clock K, until both clocks reunite.
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Phase 1: Rocket (with clock K') embarks with constant proper acceleration a during a time Ta as measured by clock K until it reaches some velocity V. Phase 2: Rocket keeps coasting at velocity V during some time Tc according to clock K. Phase 3: Rocket fires its engines in the opposite direction of K during a time Ta according to clock K until it is at rest with respect to clock K. The constant proper acceleration has the value −a, in other words the rocket is decelerating.
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In his Florida days, Schrieffer enjoyed playing with homemade rockets and ham radio, a hobby that sparked an interest in electrical engineering.
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Rockets in particular can use regenerative cooling, which uses the fuel to cool the solid parts of the engine.
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The thrust provided by the engines acts at the surface of the rocket nozzle rather than acting uniformly on the spacecraft, and is transmitted through the structure of the spacecraft via compressive and tensile forces to the objects or people inside.
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Malina's thesis adviser was engineer-aerodynamicist Theodore von Kármán, who eventually arranged for United States Army financial support for this "GALCIT Rocket Project" in 1939.
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(Rocket launch) So now it's hovering at about 40 meters, and it's constantly adjusting the angle, the pitch and yaw of the main engine, and maintaining roll with cold gas thrusters.
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22 sinne gevind in 7 ms. Hulle kom uit baie bronne en word nie nagegaan nie.