Performance assessment of a Space Station rescue and personnel/logistics vehicle
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26109
Reference3 articles.
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Deorbit Options for a Low Lift-to-Drag Ratio Space Emergency Rescue Vehicle;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2017
2. Launch pad abort of the HL-20 lifting body;Journal of Guidance, Control, and Dynamics;1994-11
3. Preliminary structural evaluation and design of the HL-20;Journal of Spacecraft and Rockets;1993-09
4. Optimal return-to-launchsite abort trajectories for an HL-20 Personnel Launch System vehicle;Flight Simulation and Technologies;1993-08-09
5. Aerodynamic characteristics of the HL-20 and HL-20A lifting-body configurations;9th Applied Aerodynamics Conference;1991-08-17
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