Entry Configurations and Performance Comparisons for the Mars Smart Lander-Reference-Cited by-同舟云学术

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Entry Configurations and Performance Comparisons for the Mars Smart Lander

Published:2002-06-25 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference and Exhibit
language:
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Author:

Lockwood Mary Kae¹,Sutton Kenneth¹,Prabhu Ramadas¹,Powell Richard¹,Graves Claude²,Epp Chirold²,Carman Gilbert²

Affiliation:

1. NASA Langley Research Center

2. NASA Johnson Space Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-4407

Reference18 articles.

1. An atmospheric guidance algorithm testbed for the Mars Surveyor Program 2001 Orbiter and Lander

2. Mars Smart Lander Simulations for Entry, Descent, and Landing

Cited by 13 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Supersonic Aerodynamic Characteristics of Blunt Body Trim Tab Configurations;31st AIAA Applied Aerodynamics Conference;2013-06-22

2. Hypersonic and Supersonic Static Aerodynamics of Mars Science Laboratory Entry Vehicle;43rd AIAA Thermophysics Conference;2012-06-25

3. Transition Analysis for the Mars Science Laboratory Entry Vehicle;41st AIAA Thermophysics Conference;2009-06-14

4. Erratum on Laminar-Turbulent Transition on Reentry Capsules and Planetary Probes;Journal of Spacecraft and Rockets;2007-03

5. Laminar-Turbulent Transition on Reentry Capsules and Planetary Probes;Journal of Spacecraft and Rockets;2006-11

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