Minimum Impulse Trajectories with Specified Transfer Time
Keywords: Rocket, Circular Orbits, Transfer Trajectories
AbstractTransfer Trajectories between circular orbits in an inverse square gravitational field are investigated, the criterion of optimization adopted being minimization of total impulse velocity applied at the terminals with flight time of the rocket serving as a constraint.
How to Cite
Srivastava, T., & Singh, M. (2014). Minimum Impulse Trajectories with Specified Transfer Time. Defence Science Journal, 21(3), 175-178. https://doi.org/10.14429/dsj.21.6247
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