Testing of SLA-561V in NASA-Ames Turbulent Flow Duct With Augmented Radiative Heating-Reference-Cited by-同舟云学术

Testing of SLA-561V in NASA-Ames Turbulent Flow Duct With Augmented Radiative Heating

Published:2011-06-14 Issue: Volume: Page:
ISSN:
Container-title:42nd AIAA Thermophysics Conference
language:
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Author:

Sepka Steven¹,Wray Alan²,Prabhu Dinesh¹,Kornienko Robert²,Radbourne Chris²

Affiliation:

1. ERC, Inc.

2. NASA Ames Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3619

Reference20 articles.

1. Wright, M., Beck, R., Edquist, K., Driver, D., Sepka, S., Slimko, E., Willcockson, W., DeCaro, A., Hwang, H. "Sizing and Margins Assessment of the Mars Science Laboratory Aeroshell Thermal Protection System," AIAA PaperNo.2009-4231,June2009.

2. Edquist,K.T.,Dyakonov, A.,WrightM.J.,and Tang, C.Y. "Aerothermodynamic Environments Definition for the Mars ScienceLaboratoryEntryCapsuleAIAAPaperNo.2007-1206,January2007.

3. Edquist, K.T., Dyakonov, A., Wright M.J., and Tang, C.Y. "Aerothermodynamic Design of the Mars Science LaboratoryHeatshield,"AIAA Paper No.2009-4075,June2009.

4. Driver, D., Carballo, J. E., Beck, R., Prabhu, D., Santos, J., Slimko, E., Willcockson, W., Songer, J. "Arc Jet Testing in a Shear Environment for Mars Science Laboratory Thermal Protection System" AIAA Paper No. 2009-4230,June2009.

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