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Deployable self-regulating centrifugally-stiffened decelerator (DESCENT): Design scalability and low altitude drop test

  • Published:2021-07 Issue: Volume:114 Page:106710
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Wu RuiORCID,Roberts Peter C.E.,Xu Lulu,Soutis ConstantinosORCID,Diver Carl

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference44 articles.

1. Mars exploration entry, descent, and landing challenges;Braun;J. Spacecr. Rockets,2007

2. High mass Mars entry, descent, and landing architecture assessment;Steinfeldt,2009

3. Human exploration of Mars, design reference architecture 5.0;Drake,2010

4. Aerodynamic decelerators for planetary exploration: past, present, and future;Cruz,2006

5. Mission sizing and trade studies for low ballistic coefficient entry systems to Venus;Dutta,2012

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