Analytical study of longitudinal perturbations to steady orbital flight of lifting self-propelled vehicle in circular orbit; calculations are performed with linear and nonlinear equations for set of aerodynamic and inertial parameters, and altitudes from 100,000 to 700,000 ft; applicability to entry or glide phase and to sustained flight of self-propelled sub-satellite describing steady circular orbit.
Longitudinal dynamics of lifting vehicle in orbital flight
J Aerospace Sciences
Journal of Aerospace Sciences ; 28 , n 10
1961
Aufsatz (Zeitschrift)
Englisch
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