Design and testing of an upper stage hybrid propulsion system using hydrogen peroxide oxidizer
36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit ; 2000 ; Las Vegas , NV , U.S.A.
01.01.2000
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Design and Testing of an Upper Stage Hybrid Propulsion System Using Hydrogen Peroxide Oxidizer
British Library Conference Proceedings | 2000
|Hydrogen Peroxide as an Alternate Oxidizer for a Hybrid Rocket Booster
Online Contents | 1995
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