Evaluation of High-Temperature Multilayer Insulation for Inflatable Ballute
Author:
Affiliation:
1. Lockheed Martin Space Systems Company, Denver, Colorado 80201
2. ILC Dover, Inc., Frederica, Delaware 19934
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3728
Reference4 articles.
1. Aeroassist Systems: An Important Element in NASA's New Era of Planetary Exploration
2. Development status of attached inflatable decelerators.
3. Attached inflatable ballute for spacecraft deceleration
Cited by 4 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. Fluid–Structure Interaction Simulations of a Tension-Cone Inflatable Aerodynamic Decelerator;AIAA Journal;2013-07
2. Structural and Control Concepts for Variable Geometry Planetary Entry Systems;50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2009-05-04
3. Ballute Entry Systems for Lunar Return and Low-Earth-Orbit Return Missions;Journal of Spacecraft and Rockets;2008-05
4. An Evaluation of Ballute Entry Systems for Lunar Return Missions;AIAA Atmospheric Flight Mechanics Conference and Exhibit;2006-06-25
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