TANDEM: Tension Adjustable Network for Deploying Entry Membrane-Reference-Cited by-同舟云学术

TANDEM: Tension Adjustable Network for Deploying Entry Membrane

Published:2018-11 Issue:6 Volume:55 Page:1379-1392
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Schroeder Kevin¹,Samareh Jamshid²,Bayandor Javid³

Affiliation:

1. CRashworthiness for Aerospace Structure and Hybrids (CRASH) Lab Virginia Tech, Blacksburg, Virginia 24061

2. NASA Langley Research Center, Hampton, Virginia 23666

3. CRashworthiness for Aerospace Structure and Hybrids (CRASH) Lab University at Buffalo—The State University of New York, Buffalo, NY 14260

Funder

National Aeronautics and Space Administration

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A33913

Reference25 articles.

1. Adaptive Deployable Entry and Placement Technology (ADEPT): A Feasibility Study for Human Missions to Mars

2. Progress in Payload Separation Risk Mitigation for a Deployable Venus Heat Shield

3. Quasistatic shape adjustment of a 15-meter-diameter space antenna

4. TibertG. “Deployable Tensegrity Structures for Space Applications,” Ph.D. Dissertation, Dept. of Mechanics, Royal Inst. of Technology, Stockholm, Sweden, 2002.

5. Deployable Tensegrity Reflectors for Small Satellites

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