Strategies to utilize advanced heat shield technology for high-payload mars atmospheric entry missions-Reference-Cited by-同舟云学术

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Strategies to utilize advanced heat shield technology for high-payload mars atmospheric entry missions

Published:2017-07 Issue: Volume:136 Page:22-33
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Braun Max,Bruce Paul,Levis Errikos

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference28 articles.

1. Robert D. Braun, Robert M. Manning, Mars Exploration Entry, Descent and Landing Challenges, 2007.

2. Chris J. Cerimele, Jarret M. Lafleur, Mars Entry Bank Profile Design for Terminal State Optimization, 2008.

3. Mark Schoenenberger, Karl T. Edquist, Prasun N. Desai, Aerodynamics for the Mars Phoenix Entry Capsule, 2011.

4. NASA Mars Architecture Steering Group Bret G. Drake, Human Exploration of Mars Design Reference Architecture 5.0, 2009.

5. Michelle M. Munk, Overview of the nasa entry, descent, and landing systems analysis (edl-sa), 2010.

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