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...lysis of the effect of factors on the efficiency of liquid rocket turbine" by Zu, Guojun; Zhang, Yuanjun ''Journal of Propulsion Technology '' no. 6, p {{DEFAULTSORT:Rocket Turbine Engine}} ...

...the "unit of movement". Momentum is related to mass and velocity, as given by the formula ''P = mv,'' where ''P'' is the momentum, ''m'' the mass, and '' ==Rockets and rocket-like reaction engines== ...

|image = XLR-99 Rocket Engine USAF.jpg |caption = An XLR-99 rocket engine. ...

[[File:Gimbaled thrust animation.gif|thumb|right|Animation of the motion of a rocket as the nozzle is gimbaled]] '''Gimbaled thrust''' is the system of [[thrust vectoring]] used in most [[rocket]]s, including the [[Space Shuttle program|Space Shuttle]], the [[Saturn V]] ...

...ble from typically used arcjet engines are very low compared with chemical engines. ...well suited to keeping stations in orbit and can replace [[monopropellant rocket]]s. ...

{{Short description|Amateur experimental rocket group}} ...Rocket Society''', the organization's name was changed to the '''Glendale Rocket Society''' two months later. Ultimately, the society changed its name to t ...

{{Short description|Rocket engine operation method}} ...ressure fed rocket cycle.svg|thumb|right|270px|Pressure-fed rocket cycle. Propellant tanks are pressurized to directly supply fuel and oxidizer to the engine, e ...

{{More citations needed|date=December 2021}}{{short description|Rocket engine operation method}} ...ly to [[Turbopump|power the pumps]] and then discarded. Most gas-generator engines use the fuel for nozzle cooling.]] ...

...ould be a suborbital flight and would test the structural integrity of the rocket. ...t would reroute the fuel for this engine to the other engines and have the rocket burn longer to compensate for the loss of acceleration. This was used succe ...

{{Short description|Small rocket engines that help fuel settle in 0g before main engine start}} ...a [[zero-g]] situation. The resulting acceleration causes liquid in the [[rocket]]'s main tanks to settle towards the aft end, ensuring uninterrupted flow t ...

{{short description|Solid propellant motor used to augment the thrust of a rocket}} ...ore_Stage_Prep_for_Lift_Mate.jpg|thumb|[[Space Launch System|SLS]]'s solid rocket boosters]] ...

{{Short description|Rocket engine}} {{infobox rocket engine ...

{{Short description|Proposed hydrolox rocket engine intended to surpass the RS-68}} {{Infobox rocket engine ...

...op and test the rocket engines for the [[Project Apollo|Apollo]]/[[Saturn (rocket family)|Saturn]] launch vehicles and the [[Apollo Lunar Module]] that enabl ...[Mars Direct]] mission architecture, in which French's concern is resolved by devoting a separate spacecraft to the return trip, so that it can be verifi ...

{{Short description|Hydrogen peroxide rocket propellant}} .... Stabilisers used included 0.0025% [[phosphoric acid]],<ref>German Liquid Rocket Fuels, www.dtic.mil/dtic/tr/fulltext/u2/122495.pdf page 5</ref> a mixture o ...

{{Short description|Wernher von Braun rocket plan}} {{Infobox rocket ...

{{Infobox rocket stage | caption = Diagram of the S-IB first stage of the Saturn IB rocket ...

{{Short description|Rocket that burns 3 propellants at once or 2 fuels with an oxidizer, sequentially} ...ave been tested by [[Rocketdyne]] and [[NPO Energomash]], no tripropellant rocket has been flown. ...

{{Infobox rocket |image = File:Daniel (rocket).gif <!--image filename (omit "Image:" prefix), required--> ...

...Display Shell Rocket by, Phantom Fireworks.png|thumb|1.4 Consumer Display Rocket]] ...which instead rotate for stability or are shot out of a tube; and [[bottle rocket]]s, smaller fireworks &ndash; 1½ in (3.8&nbsp;cm) long, though the attached ...