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Title: Effects of rocket-engine design parameters on regenerative-cooling capabilities of several propellants. [Propellant combinations considered were H/sub 2/--F/sub 2/, H/sub 2/--O/sub 2/, N/sub 2/H/sub 4/--F/sub 2/, NH/sub 3/--F/sub 2/, and JP4--O/sub 2/]

Technical Report ·
OSTI ID:5052898
; ;

OSTI ID:
5052898
Report Number(s):
NASA-TN-D-66
Country of Publication:
United States
Language:
English

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Related Subjects

08 HYDROGEN
10 SYNTHETIC FUELS
ROCKET ENGINES
FLUORINE
PERFORMANCE
HYDROGEN FUELS
OXYGEN
HYDRAZINE
AMMONIA
COOLING
DESIGN
FUELS
PROPELLANTS
CRYOGENIC FLUIDS
ELEMENTS
ENGINES
FLUIDS
HALOGENS
HYDRIDES
HYDROGEN COMPOUNDS
NITROGEN COMPOUNDS
NITROGEN HYDRIDES
NONMETALS
SYNTHETIC FUELS
080600* - Hydrogen- Industrial & Commercial Use- (-1989)
090310 - Inorganic Hydrogen Compound Fuels- Properties- (1976-1989)