Integrated Thermal Analysis Trades Studies of a Reusable Booster Experiment Test Vehicle-Reference-Cited by-同舟云学术

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Integrated Thermal Analysis Trades Studies of a Reusable Booster Experiment Test Vehicle

Published:2011-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA SPACE 2011 Conference & Exposition
language:
Short-container-title:

Author:

Stumph Herbert¹,Frede Michael¹,Zweber Jeffrey²,Morris Seth¹,Erdahl Dathan¹

Affiliation:

1. University of Dayton Research Institute

2. U.S. Air Force

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-7126

Reference8 articles.

1. Bradford, J., and Hellman, B. M. "Return to Launch Site Trajectory Options for a Reusable Booster without a Secondary Propulsion System," AIAA2009-6439.

2. Hellman,B.M."ReturntoLaunchSiteTrajectoryAeroheatingforaReusableBooster,"AIAA2007-6151.

3. 5SolidWorks,SoftwarePackage,Ver.2011SP4.0,DassaultSystèmes,Concord,MA.

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