Effect of thrust per element on combustion stability characteristics of hydrogen--oxygen rocket engines
Technical Report
·
OSTI ID:5174807
None
- Research Organization:
- National Aeronautics and Space Administration, Cleveland, Ohio (USA). Lewis Research Center
- OSTI ID:
- 5174807
- Report Number(s):
- N-68-36515; NASA-TN-D-4851
- Country of Publication:
- United States
- Language:
- English
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