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Incidence Stability of Space Shuttles During Re-Entry
Published online by Cambridge University Press: 07 June 2016
Summary
The equations of motion of a vehicle entering the earth’s atmosphere (space shuttle) are expanded to give the incidence oscillation equation. The stability conditions for small free oscillations are deduced. These stability conditions apply equally to short-period and long-period oscillations. A special case of critical damping is investigated and more explicit stability conditions are derived for that case.
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- Research Article
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- Copyright
- Copyright © Royal Aeronautical Society. 1974
References
1
Loh, W H T, et al
Re-entry and Planetary Entry Physics and Technology, Vol I, p 135, Springer, New York, 1968.Google Scholar
2
Furniss, T, A Source Book of Rockets, Spacecraft and Spacemen, p 115, Ward Lock, London, 1973.Google Scholar
3
Laitone, E V, Coakley, T J, Nonlinear dynamic stability of space vehicles entering or leaving an atmosphere. Presented at the Third International Congress of the Aeronautical Sciences, Paper No ICAS-20, 1962.Google Scholar
4
Arho, R, On the rotation of the orbital plane during ballistic re-entry. Planetary and Space Science, Vol 19, pp 1215–1224, 1971.CrossRefGoogle Scholar
6
Leitmann, G, On the stability of solutions of a nonlinear nonautonomous equation. International Journal of Non-Linear Mechanics, Vol I, pp 291–292, December 1966.CrossRefGoogle Scholar