An Overview of the Guided Parafoil System Derived from X-38 Experience
Author:
Affiliation:
1. NASA Johnson Space Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-1652
Reference10 articles.
1. 2Bennett, T. and Fox, R. "Design, Development & Flight Testing of the NASA X-38 7,500 Ft2Parafoil Recovery System", AIAA-2003-2107,17thCEAS/AIAAAerodynamicDeceleratorSystemsConference,May19-22,2003
2. Testing of Parafoil Autonomous Guidance, Navigation & Control for X-38
3. 4Bennett, T. and Fox, R. "Design, Development & Flight Testing of the U.S. Army 4200 Ft2Parafoil Recovery System", AIAA-2005-1628,18thCEAS/AIAAAerodynamicDeceleratorSystemsConference,May2005
4. 5Bennett, T. and Smith, J., and Fox, R. "Testing and Development of the NASA X-38 Parafoil Upper Surface Energy Modulator",AIAA-99-1753,15thCEAS/AIAAAerodynamicDeceleratorSystemsConference,June1999
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