Return to Launch Site Trajectory Aeroheating for a Resuable Booster-Reference-Cited by-同舟云学术

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Return to Launch Site Trajectory Aeroheating for a Resuable Booster

Published:2007-06-18 Issue: Volume: Page:
ISSN:
Container-title:AIAA SPACE 2007 Conference & Exposition
language:
Short-container-title:

Author:

Hellman Barry¹

Affiliation:

1. U.S. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-6151

Reference13 articles.

1. "Operationally Responsive Space Access (ORS) Call for Proposals". BAA-06-01-PKD, Air Force Material

2. Hellman, B. "Hybrid Launch Vehicle Staging OptimizationforMinimumCost." AIAA2006-7259

3. Hartong,Alicia., Rooney, Brendan. Near-Term RLVOptions. AIAA2004-5947.

4. RD-180.www.pratt-whitney.com/prod_space_rd180.asp. Lastvisited inMay2006.

Cited by 2 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. High-altitude and Low-speed Reentry Guidance for Suborbital Reusable Launch Vehicle Returning to Launch Site;21st AIAA International Space Planes and Hypersonics Technologies Conference;2017-03-02

2. Critical Flight Conditions of Operational Rocketback Trajectories;AIAA SPACE 2012 Conference & Exposition;2012-09-11

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