Final Approach and Landing for a Winged Reusable Booster-Reference-Cited by-同舟云学术

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Final Approach and Landing for a Winged Reusable Booster

Published:2008-04-28 Issue: Volume: Page:
ISSN:
Container-title:15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
language:
Short-container-title:

Author:

Hellman Barry¹,Tejtel Daniel¹

Affiliation:

1. U.S. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-2566

Reference21 articles.

1. Adams,J.etal. "ARES:AffordableREusableSpacelift." AIAA2005-6682,AIAASpace2005Conference.

2. Surber,T.E.,andOlsen,D.C. "SpaceShuttleOrbiterAerodynamicDevelopment." AIAA1974-991,August1974.

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1. Configuration Determination of a Reusable First Stage Booster Utilizing Monte Carlo Based Inverse Design;AIAA SPACE 2011 Conference & Exposition;2011-06-14

2. The Sensitivities of Aerodynamic Forces and Moments of a Reusable First Stage Booster to Design Parameters;AIAA SPACE 2011 Conference & Exposition;2011-06-14

3. Experimental Investigation of a Suborbital Reusable Booster Concept with a Body Flap;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04

4. Technical Challenges for an Integrated Reusable Booster System Flight Demonstrator;AIAA SPACE 2010 Conference & Exposition;2010-06-26

5. Advanced TSTO Vessel Design for Safe and Inexpensive Human Orbital Access;AIAA SPACE 2008 Conference & Exposition;2008-06-15

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