Ballute Entry Systems for Lunar Return and Low-Earth-Orbit Return Missions
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta, Georgia 30332-0150
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.31612
Reference28 articles.
1. Inflatable Re-entry Vehicle Experiment (IRVE) Design Overview
2. Survey of Ballute Technology for Aerocapture
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1. Spectroscopy of High Speed Expanding Argon Flows;AIAA Aviation 2019 Forum;2019-06-14
2. Analysis of a Free-Fall Ballute Vehicle;53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference<BR>20th AIAA/ASME/AHS Adaptive Structures Conference<BR>14th AIAA;2012-04-23
3. Parametric Characterization of the Embedded Shock Phenomenon in Tension Cone Inflatable Aerodynamic Decelerators;21st AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar;2011-05-23
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