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U.S. Department of Energy
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Steady-state rocket combustion of gaseous hydrogen and liquid oxygen. Part II: Analysis for coaxial jet injection

Technical Report ·
OSTI ID:5240535
None
Research Organization:
Rocketdyne, Canoga Park, Calif. (USA)
OSTI ID:
5240535
Report Number(s):
N-66-14456; AFOSR-65-1319
Country of Publication:
United States
Language:
English