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[[Category:Rocket engines using the tap-off cycle]] [[Category:Rocket engines of the United States]] ...

...xide_Based_Propulsion_System_for_Micro_Air_Vehicle_Applications.pdf |title=Hydrogen Peroxide Based Propulsion System for Micro Air Vehicle Applications|accessd {{DEFAULTSORT:Rocket Turbine Engine}} ...

...m operates in order to produce [[acceleration]]. In the case of a chemical rocket, for example, the reaction mass is the [[Product (chemistry)|product]] of t ==Rockets and rocket-like reaction engines== ...

...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. ...

{{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.]] ...

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

{{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|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. ...

...cket engine]] front-end ("powerhead", sometimes also termed a [[Powerpack (rocket engine)|powerpack]]) that would utilize a [[Staged_combustion_cycle#Full-fl ...ss release |url=http://spaceref.com/news/viewpr.html?pid=20387 |title=New 'Rocket Engine of the Future' goes to 'Mainstage' |publisher=Pratt & Whitney Rocket ...

{{for|jet engines that cool but do not liquefy the air|Precooled jet engine}} ...[[Earth's atmosphere|atmosphere]]. A liquid air cycle engine uses [[liquid hydrogen]] (LH2) fuel to liquefy the air. ...

{{Short description|Storable hypergolic rocket fuel}} ...missile|ICBM]] rocket engines. '''Aerozine''' continues in wide use as a [[rocket fuel]], typically with [[dinitrogen tetroxide]] ({{Chem2|N2O4}}) as the [[o ...

During [[World War II]], [[Germany]] fielded many [[aircraft]] and [[rocket]]s whose fuels, and oxidizers, were designated (letter)-''Stoff'' ({{IPA|de ...meanings at different times; for example, '''''T-Stoff''''' meant a rocket propellant in World War II, but a [[tear gas]] ([[xylyl bromide]]) in World War I. ...

...123/https://history.nasa.gov/SP-4404/ch8-1.htm |date=2021-01-26 }}, LIQUID HYDROGEN AS A PROPULSION FUEL,1945-1959, Chapter 8.1, accessed 13.03.2021</ref> ...123/https://history.nasa.gov/SP-4404/ch8-1.htm |date=2021-01-26 }}, LIQUID HYDROGEN AS A PROPULSION FUEL,1945-1959, Chapter 8.5, accessed 13.03.2021</ref> LH2 ...

{{short description|Type of vibration in a rocket engine}} ...ion on the vehicle's flexible structure, which in turn cause variations in propellant pressure and flow rate, closing the self-excitation cycle. The name is a me ...

...e]]s; one used as the first stage and two as boosters]]{{Short description|Rocket with interchangeable components}} A '''modular rocket''' is a kind of [[multistage rocket]] which has components that can interchanged for different missions. Severa ...

...]. Gas generators of this type are used to power [[turbopump]]s in rocket engines, in a [[gas-generator cycle]]. The [[V-2 rocket]] used [[hydrogen peroxide]] decomposed by a liquid [[sodium permanganate]]<!-- Some sources ...

{{Infobox rocket stage {{Infobox rocket/Stage ...

{{short description|Space station made from a spent rocket stage}} ...ld otherwise have no further purpose, but the in-orbit modification of the rocket stage could prove difficult and expensive. {{Asof|2024|11}}, no wet-worksho ...

{{Infobox rocket {{Infobox rocket/payload ...

...ts. Alternatively, radioisotopes may be used in a '''radioisotope electric rocket''',<ref>{{cite journal |last1=Schmidt |first1=George R. |last2=Manzella |fi ...nbsp;seconds (7 to 8&nbsp;kN·s/kg), about double that of the best chemical engines such as the [[LH2]]-[[LOX]] [[Space Shuttle Main Engine]]. ...