Stability of Rocket Flight during Burning
Keywords: Gravity, Aerodynamic Forces, Torques
AbstractStability of the rocket motion during burning is discussed taking into consideration gravity, aerodynamic forces and torques. Conditions for stabilizing the rocket motion are investigated. Analysis for initial and final phases of burning is given separately. Stability regions of the projected motions on two dimensional co-ordinate planes are obtained and thereby stability region of the actual motion is derived. Stability diagrams illustrate statically and dynamically stable and unstable regions.
How to Cite
Srivastava, T., & Singh, M. (2014). Stability of Rocket Flight during Burning. Defence Science Journal, 17(4), 215-222. https://doi.org/10.14429/dsj.17.7407
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