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ADEPT Sounding Rocket One Flight Test OverviewOn September 12th 2018, a sounding rocket flight test was conducted on a mechanically-deployed atmospheric entry system known as the Adaptable Deployable Entry and Placement Technology (ADEPT). The purpose of the Sounding Rocket One (SR-1) test was to gather critical flight data for evaluating the vehicle's in-space deployment performance and supersonic stability. This flight test was a major milestone in a technology development campaign for ADEPT: the application of ADEPT for small secondary payloads. The test was conducted above White Sands Missile Range (WSMR), New Mexico on a SpaceLoft XL rocket manufactured by UP Aerospace. This paper describes the system components, test execution, and test conclusions.
Document ID
20190027649
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Cassell, Alan
(NASA Ames Research Center Moffett Field, CA, United States)
Wercinski, Paul
(NASA Ames Research Center Moffett Field, CA, United States)
Yount, Bryan
(NASA Ames Research Center Moffett Field, CA, United States)
Nishioka, Owen
(NASA Ames Research Center Moffett Field, CA, United States)
Williams, Joseph
(Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Dutta, Soumyo
(NASA Langley Research Center Hampton, VA, United States)
Korzun, Ashley
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
July 24, 2019
Publication Date
July 11, 2019
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
ARC-E-DAA-TN70404
Meeting Information
Meeting: International Planetary Probe Workshop
Location: Oxford, England
Country: United Kingdom
Start Date: July 8, 2019
End Date: July 12, 2019
Sponsors: European Space Agency (ESA)
Funding Number(s)
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Public Use Permitted.
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