Gaseous hydrogen-liquid oxygen rocket combustion at supercritical chamber pressures. [Effect of chamber pressure on rocket combustor performance was determined]
Technical Report
·
OSTI ID:5146680
None
- Research Organization:
- National Aeronautics and Space Administration, Cleveland, Ohio (USA). Lewis Research Center
- OSTI ID:
- 5146680
- Report Number(s):
- NASA-TN-D-4172
- Country of Publication:
- United States
- Language:
- English
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