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...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 ...d Evaluation of the USAF Ballistic Test Evaluation System for Solid Rocket Propellants”.<ref> ...

...ellant rockets<ref name="s94">Byron L. Cockrell, ''Ballistic Evaluation of Propellants in Micro-motors'' (1964), Report S-94 (AD451357) ([http://stinet.dtic.mil/o ...age:Clamp-Type 2C1.5-4 Motor.png|thumb|200px|Redesigned Clamp-Type 2C1.5-4 Rocket Motor used for remote testing]] ...

...''' 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 ...

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

| Rocket = Atlas V 541 this is all true ...of one day seeing humans on Mars. Oxygen isn’t just the stuff we breathe. Rocket propellant depends on oxygen, and future explorers will depend on producing ...

...h an atmosphere, and it requires less fuel than does the direct use of a [[rocket engine]]. * '''[[Aerospike engine]]''' – is a type of [[rocket engine]] that maintains its [[aerodynamic]] efficiency across a wide range ...