Special areas of rocket testing.
- 1 March 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 3 (3) , 289-301
- https://doi.org/10.2514/3.28443
Abstract
No abstract availableKeywords
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- DIFFUSER AUXILIARY EJECTOR DEVELOPMENT FOR THE DESIGN OF THE J-3 LEM DESCENT EXHAUST SYSTEMPublished by Defense Technical Information Center (DTIC) ,1966
- Fluorine propulsion technologyPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1965
- Interior ballistics of spinning solid- propellant rocketsJournal of Spacecraft and Rockets, 1965
- Multiple rocket firing unit for altitude testingJournal of Spacecraft and Rockets, 1965
- A SIMULATION APPROACH TO THE THRUST STAND DYNAMICS PROBLEMPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1964
- AUXILIARY EJECTOR EFFECTS ON ROCKET-DRIVEN DIFFUSER PERFORMANCE DURING THRUST VARIATIONPublished by Defense Technical Information Center (DTIC) ,1963