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Aerocapture Technology Demonstration Risk Reduction ActivityNASA Langley Research Center (LaRC) has developed and constructed a full-scale mockup of a trim tab mechanism for a steerable entry vehicle to address the risks associated with a Technology Demonstration Mission (TDM) with respect to the mass and volume needed for such a system as compared to existing steering systems. This paper provides an overview of the conceptual design effort and the results of the risk reduction effort.
Document ID
20240004907
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Scott Belbin
(Langley Research Center Hampton, Virginia, United States)
Nicholas Vitullo
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Date Acquired
April 18, 2024
Subject Category
Spacecraft Design, Testing and Performance
Meeting Information
Meeting: 47th Aerospace Mechanisms Symposium
Location: Virginia Beach, VA
Country: US
Start Date: May 15, 2024
End Date: May 17, 2024
Sponsors: National Aeronautics and Space Administration
Funding Number(s)
WBS: 981698.01.03.23.03
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
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