A comparison of the hypersonic vehicle fuel JP-7 to the rocket propellants RP-1 and RP-2 with the advanced distillation curve method

Energy and Fuels

Volumn 23, Issue 7, 2009, Pages 3637-3644

  Lovestead, Tara M ^a   Bruno, Thomas J ^a  

^a NATIONAL INSTITUTE OF STANDARDS AND TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR RESISTANCE; AT-SPEED; AVAILABLE ENERGY; DISTILLATION CURVES; EXTREME TEMPERATURES; FLASH POINTS; HIGH ALTITUDE; HIGH THERMAL STABILITY; HYPERSONIC AIRCRAFT; HYPERSONIC VEHICLES; OPERATIONAL DEMANDS; REPRESENTATIVE SAMPLE; ROCKET PROPELLANTS; STRINGENT REQUIREMENT; SUBSTITUTE FUELS; THERMAL STABILITY; THERMO-PHYSICAL PROPERTY;

COLD STORAGE; COMPRESSED AIR; DISTILLATION; HEAT RESISTANCE; HYDROCARBONS; HYPERSONIC AERODYNAMICS; PROPELLANTS; RECONNAISSANCE AIRCRAFT; ROCKETS; SPACECRAFT PROPULSION; THERMODYNAMIC STABILITY; VEHICLES;

FUELS;

EID: 67749148205     PISSN: 08870624     EISSN: None     Source Type: Journal    
DOI: 10.1021/ef900096q     Document Type: Article

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