Effect is investigated for Hohmann type transfers; closed form solution of trajectory during thrusting is obtained by assuming that constant thrust is applied normal to focal radius and that change of radial position of rocket is small; example shows thrusting time, thrust level, propellant consumption, and conic trajectories following powered flight paths, etc, in comparison with ordinary impulsive thrust case; calculations of lead angle and time are introduced based on analysis presented.
Effect of finite thrusting time in orbital maneuvers
AIAA J
AIAA Journal ; 1 , n 1
1963
5 pages
Article (Journal)
English
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EFFECT OF FINITE THRUSTING TIME IN ORBITAL MANEUVERS
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