A Flight Dynamics Perspective of the Orion Pad Abort One Flight Test-Reference-Cited by-同舟云学术

A Flight Dynamics Perspective of the Orion Pad Abort One Flight Test

Published:2009-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference
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Author:

Idicula Jinu¹,Williams-Hayes Peggy¹,Stillwater Ryan¹,Yates Max²

Affiliation:

1. NASA Dryden Flight Research Center

2. United States Air Force

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-5730

Reference8 articles.

1. Orion Entry, Descent and Landing Simulation

2. ANTARES: Spacecraft Simulation for Multiple User Communities and Facilities

3. 3Justus, C. G. and Johnson, D. L. "The NASA/MSFC Global Reference Atmospheric Model 1999 Version (GRAM-99)," Tech. Rep. NASA TM-1999-209630, National Aeronautics and Space Administration, 1999.

4. Crew Exploration Vehicle (CEV) Crew Module shape selection analysis and CEV Aeroscience Project Overview

5. 5Robinson, P. E. and Thompson, J. A. "Formulation of the Orion Aerodynamic Database, Revision 0.51.2," Tech. Rep. NASA EG-CEV-06-37, National Aeronautics and Space Administration, 2008.

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