Radiative and Convectiove Heating of Orion Space Vehicles at Earth Orbital Entries-Reference-Cited by-同舟云学术

Radiative and Convectiove Heating of Orion Space Vehicles at Earth Orbital Entries

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Surzhikov Sergey¹,Shang Joe²

Affiliation:

1. Russian Academy of Sciences

2. Wright State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-251

Reference16 articles.

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2. JonesW.L. Jr., CrossA.E. Electrostatic Probe Measurements of Plasma Parameters for Two Reentry Flight Experimentsat25000 Feetper Second.NASATND-6617.1972.

3. Reid R.C., Rochelle W.C., Milhoan J.D. Radiative Heating to the Apollo Command Module: Engineering PredictionsandFlightMeasurements.NASATM-58091.1972.

4. NASA's ExplorationSystems Architecture.FinalReport.NASA-TM-2005-214062.November 2005.758p.

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