An Integrated Six Degree-of-Freedom Trajectory Simulator for Hybrid Sounding Rockets
Author:
Affiliation:
1. University of KwaZulu-Natal
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-1223
Reference14 articles.
1. Status Update Report for the Peregrine Sounding Rocket Project: Part III
2. Preliminary Design of a Hybrid Propulsion Multimission Missile System
3. General theory of optimal trajectory for rocket flight in a resisting medium
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