DSMC Simulations of Ballute Aerothermodynamics Under Hypersonic Rarefied Conditions-Reference-Cited by-同舟云学术

DSMC Simulations of Ballute Aerothermodynamics Under Hypersonic Rarefied Conditions

Published:2005-06-06 Issue: Volume: Page:
ISSN:
Container-title:38th AIAA Thermophysics Conference
language:
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Author:

Moss James¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-4949

Reference18 articles.

1. Jahemenko, I. M. \Ballute Characteristics in the 0.1 to 10 Mach Number Speed Range," Journal of Spacecraft, Vol.4, No.8,pp.1058-1063,August1967.

2. Guy,L.D.\StructuralandDeceleratorDesignOptionsforMarsEntry,"Journal of Spacecraft, Vol.6,No.1,pp.44-49, January1969.

3. McRonald,A.D.\ALight-weightIn atableHypersonicDragDeviceforHypersonicEntry,"presentedattheAssociation AeronautiquedeFranceConferenceat Arcachon,France,March,1999.

4. Hall,J.L.,andLe,A.K.\AerocaptureTrajectoriesforSpacecraftwithLarge,TowedBallutes,"AAS/AIAASpaceFlight MechanicsMeeting,February2001,PaperAAS01-235.

5. Miller, K. L., Gulick, D., Lewis, J., Trochman, B., Stein, J., Lyons, D. T., and Wilmoth, R. G. \Trailing Ballute Aerocapture: Concept andFeasibilityAssessment,"AIAAPaper2003-4655,July2003.

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