Design and Execution of the Hypersonic Inflatable Aerodynamic Decelerator Large-Article Wind Tunnel Experiment-Reference-Cited by-同舟云学术

Design and Execution of the Hypersonic Inflatable Aerodynamic Decelerator Large-Article Wind Tunnel Experiment

Published:2013-03-23 Issue: Volume: Page:
ISSN:
Container-title:AIAA Aerodynamic Decelerator Systems (ADS) Conference
language:
Short-container-title:

Author:

Cassell Alan¹,Swanson Gregory T.²,Quach Bill¹,Kushner Laura K.¹,Brown Jeffrey D.²,Kazemba Cole D.³,Kruger Carl¹,Johnson Roger K.⁴,Hughes Stephen J.⁴,Littell Justin⁴,Calomino Anthony M.⁴,Cheatwood F. M.⁴

Affiliation:

1. NASA Ames Research Center

2. ERC, Inc.

3. Science and Technology Corporation

4. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-1304

Reference12 articles.

1. Overview of the NASA Entry, Descent and Landing Systems Analysis Stud

2. Hypersonic Inflatable Aerodynamic Decelerator (HIAD)Technology Development Overview

3. Wright, H., Cuttright, A., Corliss, J., Bruce, W., Trombetta, D., Mazaheri, A. R., Coleman, M., Olds, A., Hancock, S. "HEARTFlight TestOverview,"9thInternationalPlanetaryProbeWorkshop,16-22June,2012,Toulouse,France.

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