Maximum Atmospheric Entry Angle for Specified Retrofire Impulse
Keywords: Retrofire impulse, Elliptic orbits
AbstractMaximum atmospheric entry angles for vehicles initially moving in elliptic orbits are investigated and it is shown that tangential retrofire impulse at the apogee results in the maximum entry angle. Equivalence of maximizing the entry angle and minimizing the retrofire impulse is also established.
How to Cite
Srivastava, T., & Nagpal, O. (2014). Maximum Atmospheric Entry Angle for Specified Retrofire Impulse. Defence Science Journal, 19(3), 177-182. https://doi.org/10.14429/dsj.19.7487
Copyright (c) 2016 Defence Science Journal
where otherwise noted, the Articles on this site are licensed under Creative Commons License: CC Attribution-Noncommercial-No Derivative Works 2.5 India