Experimental Measurement of RCS Jet Interaction Effects on a Capsule Entry Vehicle-Reference-Cited by-同舟云学术

Experimental Measurement of RCS Jet Interaction Effects on a Capsule Entry Vehicle

Published:2008-01-07 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Buck Gregory¹,Watkins A.¹,Danehy Paul¹,Inman Jennifer¹,Alderfer David¹,Dyakonov Artem¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-1229

Reference13 articles.

1. Buck, G. M., Watkins, A. N. and Danehy, P. M. "Aerothermodynamic Testing of RCS Jet Interactions on Apollo and Orion-type Crew Modules in the NASA Langley 31-Inch Mach 10 Air Tunnel: Test 37-CH," CEV AeroscienceProject Technical Brief, EG-CAP-07-97,2007.

2. Danehy, P. M., Wilkes, J. A., Brauckmann, G., Alderfer, D. W., Jones, S. B., and Patry, D. "Visualization of a Capsule Entry Vehicle Reaction-ControlSystem(RCS) Thruster"AIAA Paper 2006-1532,January 2006.

3. Danehy, P. M., Inman (Wilkes), J. A., Alderfer, D. W., and Buck, G. M. "Visualization of Flowfield Modification by RCSJetson a Capsule Entry Vehicle"AIAA Paper 2008-1231,January 2008.

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