THEORETICAL PERFORMANCE OF ROCKET ENGINES USING GASEOUS HYDROGEN IN THE IDEAL STATE AT STAGNATION TEMPERATURES UP TO 200,000 R. Report No. E-910093-30.
Technical Report
·
OSTI ID:4467659
- Research Organization:
- United Aircraft Corp., East Hartford, Conn. Research Labs.
- NSA Number:
- NSA-21-002868
- OSTI ID:
- 4467659
- Report Number(s):
- NP--16339
- Country of Publication:
- United States
- Language:
- English
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