Free-Flight Rocket Attitude Motion Due to Transverse Vibration
- 1 September 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 17 (5) , 425-431
- https://doi.org/10.2514/3.57761
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Missile stability using finite elements - An unconstrained variational approachAIAA Journal, 1976
- Dynamics of Sounding Rockets at BurnoutJournal of Spacecraft and Rockets, 1974
- General motion of a variable-mass flexible rocket with internal flowJournal of Spacecraft and Rockets, 1970
- Calculated aeroelastic bending of a sounding rocket based on flight data.Journal of Spacecraft and Rockets, 1967
- On the dynamic characteristics of a variable- mass slender elastic body under high accelerations.AIAA Journal, 1967
- Dynamic stability of a flexible missile under constant and pulsating thrustsAIAA Journal, 1965