Characterization of hybrid rocket internal heat flux and HTPB fuel pyrolysis
Author:
Affiliation:
1. JPL, Pasadena, CA
2. Cohen Professional Services, Redlands, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1994-2876
Reference7 articles.
1. RocketRopulsion?", EumpeanSpaceAgency,Bordeaux,France, lune 1991.
2. "WhatistheF u m ofHybridRocketFmpulsionforU.S.Space LaunchSystems?",Position PaperbytheNationalSpace Propulsion SynergyGmup,1992dnft
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