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ADEPT SR-1 Flight ExperimentThe ADEPT architecture represents a completely new approach for entry vehicle design using a high-performance carbon fabric to serve as the primary drag surface of the mechanically deployed decelerator and to protect the payload from hypersonic aerothermal heating during entry. The initial system-level development of the nano-ADEPT architecture will culminate in the launch of a 0.7-m deployed diameter ADEPT sounding rocket flight experiment. The SR-1 sounding rocket flight experiment is a critical milestone in the technology maturation plan for ADEPT and will generate performance data on in-space deployment and aerodynamic stability.
Document ID
20170001940
Acquisition Source
Ames Research Center
Document Type
Other - Brief Communication/Note
Authors
Wercinski, Paul F.
(NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
March 2, 2017
Publication Date
February 1, 2017
Subject Category
Engineering (General)
Report/Patent Number
NASA FS-2017-02-01-ARC
ARC-E-DAA-TN39114
Funding Number(s)
WBS: WBS 513851
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
aeroshell
deployable
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