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...d Evaluation of the USAF Ballistic Test Evaluation System for Solid Rocket Propellants”.<ref> ...d Evaluation of the USAF Ballistic Test Evaluation System for Solid Rocket Propellants Accession Number : AD0276424: Technical documentary report : TEST GROUP (DE ...

...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 ...y hazardous materials.<ref name="s94"/> Due to the hazardous nature of the propellants, Cockrell had to design casting equipment and facilities that could be oper ...

|journal=Propellants, Explosives, Pyrotechnics |journal=Propellants, Explosives, Pyrotechnics ...

...well |first3=B. J. |date=2002-05-01 |title=Combustion of Liquefying Hybrid Propellants: Part 1, General Theory |url=https://arc.aiaa.org/doi/10.2514/2.5975 |journ ...f name=":4">An Investigation of Injectors for Use with High Vapor Pressure Propellants with Applications to Hybrid Rockets. BS Waxman. Stanford University, 2014.< ...

...W.H. Andersen & N.A. Louie, “Projectile Impact Ignition Characteristics of Propellants I. Deflagrating Composite Explosive,” ''Combustion Science and Technology'' ...

...ane L.|date=September–October 2001|title=Mars Rocket Vehicle Using In Situ Propellants|journal=Journal of Spacecraft and Rockets|volume=38|issue=5|pages=730–735|b ...

...rip Biaxial Tension Specimen for a HTPB-Based Propellant Material |journal=Propellants, Explosives, Pyrotechnics |date=1999 |volume=24 |issue=6 |pages=349–352 |do ...

...opellant rocket is a [[rocket]] with a [[rocket motor]] that uses [[rocket propellants]] in two different phases: [[solid rocket propellant|one solid]] and the ot ...pellant]] from the tanks into the combustion chamber, which means that the propellants can be kept under low pressure. This permits the use of low-mass propellant ...