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{{Short description|Rocket engine}} ...[[reduction oxidation|redox]] ([[combustion]]) reaction as in a [[chemical rocket]]. ...

...eb|last=Thuloweit |first=Kenji |title=AFRL test marks return to 'in-house' rocket fuel development |url=http://www.af.mil/news/story.asp?id=123213934 |work=P ...ment and Evaluation of the USAF Ballistic Test Evaluation System for Solid Rocket Propellants”.<ref> ...

...bustion instability|combustion instabilities]] in systems such as [[rocket engines]], etc.<ref name="williams">Williams, F. A. (2018). Combustion theory. CRC ...

...2</ref> "Flight" gives examples of these internal forces for two early jet engines, the [[Rolls-Royce Avon]] Ra.14<ref>{{cite web|url=https://www.flightglobal ...he net thrust of the engine. Consequently, the thrust characteristics of a rocket motor are different from that of an air breathing jet engine, and thrust is ...

...ing through the nozzle. A MET’s heating feature is like one of an [[Arcjet rocket|arc-jet]] (another propulsion device); however, due to the free-floating pl [[Thrust]] is the force that is applied on the rocket caused by when the propellant is released. The formula for thrust is given ...

...tions like [[aircraft engines]], [[internal combustion engines]], [[rocket engines]], industrial furnaces, and power station combustors. The simple chemical r ...

{{Short description|Soviet (now Russian) liquid rocket engine}} {{infobox rocket engine ...

...acoustic instabilities are a major hazard to [[gas turbines]] and [[rocket engines]].<ref name="culick-06" /> Moreover, flame blowoff of an aero-gas-turbine ...ame="pempie-01">{{cite journal|last=Pempie, P. and Vernin, H.|title=Liquid rocket engine test plan comparison |journal=AIAA Paper 2001-3256}}</ref> are large ...

...''' refers to the process by which the fuel grain of a [[hybrid-propellant rocket]] is converted from a solid to a gas that is combusted. It encompasses the Because the quantity of [[Rocket propellant|fuel]] being burned is important for the effectiveness of combus ...

...iffusion]] flames (e.g. furnaces, turbo-machinery, some liquid-fuel rocket engines and [[internal combustion engine]]s) depending on the nature of mixed gas f ...

...pulse (physics)|impulsive]] [[thrust]]s produced by traditional [[chemical rocket]]s. For the first half of the journey the propulsion system would constantl ...baez/physics/Relativity/SR/Rocket/rocket.html Baez, UCR, "The relativistic rocket"]</ref> ...

...onventional impulsive transfers in the orbit which uses thermal [[rocket]] engines to develop impulse of the order of 300-400s. Such type of transfer uses low ...

...with the +''x_b'' direction. Other types of aircraft, such as [[rocket]]s and airplanes that use [[thrust vectoring]], can have significant compon ...

...s-lunar injection]] (TLI) orbit by the under-development [[Long March 10]] rocket. The lander-propulsion stage arrangement is somewhat analogous to the lande ...and other mission segments have been constructed and the requisite rocket engines are undergoing hot fire tests. Lin further elaborated that prototype produc ...

[[File:Apollo 17 The Last Moon Shot Edit ro.jpg|thumb|A [[Saturn V]] rocket, one of the most [[Impulse (physics)|powerful]] operational launch vehicles | colspan="2" | [[Angara (rocket)|Angara]] ...

...minated by combustion products. Working fluids for ''external'' combustion engines include air, hot water, [[pressurized water reactor|pressurized water]] or ...r of the diesel engine, [[Rudolf Diesel]], was using peanut oil to run his engines.<ref>{{cite journal |last1=Shay |first1=E.Griffin |title=Diesel fuel from v ...

...ire-up.jpg|thumb|The [[Project Rover#Kiwi A|Kiwi-A Prime]] nuclear thermal rocket engine 1960 test at [[Jackass Flats]], Nevada.]] ...6-02-23}}</ref> One of the more explored concepts is the [[nuclear thermal rocket]], which was ground tested in the [[NERVA]] program. [[Nuclear pulse propul ...

...ove the ground in one place stays in one place thanks to the thrust of its engines). ...

...ok|author=George P. Sutton|author2=Oscar Biblarz|name-list-style=amp|title=Rocket Propulsion Elements|edition=7th|publisher=[[Wiley Interscience]]|date=2001| ...

...ocket engine nozzle|rocket nozzles]].<ref>{{Cite journal |date=1957 |title=Rocket Propulsion Elements. 2nd edition. George P. Sutton. J. Wiley and Sons Inc., ...e=Application of Bethe-Zel'dovich-Thompson fluids in organic Rankine cycle engines |url=http://dx.doi.org/10.2514/6.1999-462 |journal=37th Aerospace Sciences ...