Investigation of large scale parafoil rigging angles - Analytical and drop test results

Author:

Iacomini C.1,Madsen C.1

Affiliation:

1. NASA, Johnson Space Center, Houston, TX

Publisher

American Institute of Aeronautics and Astronautics

Reference12 articles.

1. [l] Muratore,J.F. andIacomini,C. S."Parafoil Flight Testof X-38 PrototypeCrewReturnVehicleYields ImprovedInstrumentationandTechniques0022,The ITEA Journalof TestandEvaluation,Volume 19, Number2,July/June1998.

2. Stein J.,Machin,R. andMuratore,J."An Overviewof theX-38 PrototypeCrewReturn VehicleDevelopmentandTestProgram0022,AIAA99-1704,(1999)

3. Smith,J.andBennet,T. "Developmentof the NASA X-38 ParafoilLandingSystem0022,m-99-1730,(1999).

4. WaSes,W.K. "AdvancedRecoverySystemsfor AdvancedLaunchVehicles(ARS). Phase1Study Results.0022,A&4-89-0881~CP (1989)

5. Lingard,J.S.,Gliding Parachutes,Parachutes q SystemsTechnologyShortCourse,Minneapolis, Minnesota,October,1998.

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