Combustion response of hydrazine-nitrogen tetroxide hypergolic rocket propellants to transverse gas flows, noting coupled and uncoupled oscillations
Hydrazine-nitrogen tetroxide combustion response to transverse gas flows.
INTERAGENCY CHEMICAL ROCKET PROPULSION GROUP, COMBUSTION CONFERENCE ; 1968 ; HOWARD COUNTY, MD
1968-10-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Numerical Study of Hydrazine and Nitrogen Tetroxide Combustion in small Rocket Motors
British Library Conference Proceedings | 1994
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