Effects of unsymmetrical stability derivative characteristics on re-entry vehicle transient angular motion
- 1 February 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 13 (2) , 82-90
- https://doi.org/10.2514/3.27887
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Effects of Unsymmetrical Stability Derivative Characteristics on Re-Entry Vehicle Trim Angle BehaviorJournal of Spacecraft and Rockets, 1974
- Aerodynamics of a Slender Cone with Asymmetric Nose Bluntness at Mach 14AIAA Journal, 1972
- Persistent re-entry vehicle roll resonancePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1966
- Dynamics of Flight: Stability and ControlPhysics Today, 1959