Launch Vehicle Gust Penetration Loads
- 1 January 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 9 (1) , 19-25
- https://doi.org/10.2514/3.61625
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
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- A mathematical model for flexible response of uprated Saturn I to inflight winds.Journal of Spacecraft and Rockets, 1968
- Wind penetration effects on flight simulationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- Effects and importance of penetration and growth of lift on space vehicle responsePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- Aeroelastic instability caused by slender payloads.Journal of Spacecraft and Rockets, 1967
- Analysis of flow separation effects on the dynamics of a large space boosterJournal of Spacecraft and Rockets, 1965
- Determination of launch-vehicle response to detailed wind profilesJournal of Spacecraft and Rockets, 1965