Thermodynamic properties and theoretical rocket performance of hydrogen to 100,000/sup 0/K and 1. 01325 X 10/sup 8/ N/m/sup 2/
Technical Report
·
OSTI ID:5190242
None
- Research Organization:
- National Aeronautics and Space Administration, Cleveland, Ohio (USA). Lewis Research Center
- OSTI ID:
- 5190242
- Report Number(s):
- NASA-SP-3069
- Country of Publication:
- United States
- Language:
- English
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Related Subjects
08 HYDROGEN
080600* -- Hydrogen-- Industrial & Commercial Use-- (-1989)
080800 -- Hydrogen-- Properties & Composition
CRYOGENIC FLUIDS
ELEMENTS
FLUIDS
FUELS
HYDROGEN
HYDROGEN FUELS
NONMETALS
PERFORMANCE
PHYSICAL PROPERTIES
ROCKETS
SYNTHETIC FUELS
THERMODYNAMIC PROPERTIES
ULTRAHIGH TEMPERATURE
080600* -- Hydrogen-- Industrial & Commercial Use-- (-1989)
080800 -- Hydrogen-- Properties & Composition
CRYOGENIC FLUIDS
ELEMENTS
FLUIDS
FUELS
HYDROGEN
HYDROGEN FUELS
NONMETALS
PERFORMANCE
PHYSICAL PROPERTIES
ROCKETS
SYNTHETIC FUELS
THERMODYNAMIC PROPERTIES
ULTRAHIGH TEMPERATURE