Minimum Impulse Trajectories with Specified Transfer Time

Authors

  • T. N. Srivastava Defence Science Laboratory, Delhi
  • Manak Singh Defence Science Laboratory, Delhi

DOI:

https://doi.org/10.14429/dsj.21.6247

Keywords:

Rocket, Circular Orbits, Transfer Trajectories

Abstract

Transfer 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.

Downloads

Published

2014-07-01

How to Cite

Srivastava, T. N., & 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

Issue

Vol. 21 No. 3

Section

General Papers

License

 Where otherwise noted, the Articles on this site are licensed under Creative Commons License: CC Attribution-Noncommercial-No Derivative Works 2.5 India