Testing and development of the NASA X-38 Parafoil Upper Surface Energy Modulator-Reference-Cited by-同舟云学术

Testing and development of the NASA X-38 Parafoil Upper Surface Energy Modulator

Published:1999-06-08 Issue: Volume: Page:
ISSN:
Container-title:15th Aerodynamic Decelerator Systems Technology Conference
language:
Short-container-title:

Author:

Bennett Thomas¹,Smith John¹,Fox Roy²

Affiliation:

1. Pioneer Aerospace Corp., South Windsor, CT

2. Aerospace Recovery Services, Belleville, WV

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-1753

Reference4 articles.

1. mith, J.,Bennett,T. andFox,R, "Developmentof theNASA X-38 ParafoilLandingSystem"Paper99-1730tobepresentedat 15* CEAS/AIAA AerodynamicDeceleratorSystemsConference& Seminar,Toulouse,France,June1999.

2. 2Stein,J.andMachin, R andMuratore,J."An OverviewoftheX-38 PrototypeCrewReturnVehicle , DevelopmentandTestProgram"Papertobepresented at 15"CEAS/AIAA AerodynamicDecelerator SystemsConference& Seminar,Toulouse,France, June1999. atel,S.,Hackett,N., andJorgensen,D. "Qualification oftheGuidedParafoilAir Delivery System- Light (GPADS-Light)"Paper97-1493 presentedat 14*AIAA AerodynamicDecelerator SystemsTechnologyConference,SanFrancisco,CA, June1997.

3. 4Machin,R andFitzgerald,SandRoyall,P.and Walter, M. "Techniquefor MeasuringPa&oil DeploymentandSteadyStateLoadsin theDispersion RisersandLeadingEdgeReinforcementTape"Paper tobepresentedat 15* CEASIAIAA Aerodynamic DeceleratorSystemsConference& Seminar,Toulouse, France,June1999.

4. so.5 30.75 31 3125 31.5 31.75 n 3225 325 s2-15 33 33% 23.5 33.75 34

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