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ADEPT Sounding Rocket One (SR-1)Flight Experiment OverviewThe SR-1 flight experiment will demonstrate most of the primary end-to-end mission stages including: launch in a stowed configuration, separation and deployment in exo-atmospheric conditions, and passive ballistic re-entry of a 70-degree half-angle faceted cone geometry.
Document ID
20170002062
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Wercinski, Paul (NASA Ames Research Center Moffett Field, CA United States)
Smith, B. (NASA Ames Research Center Moffett Field, CA United States)
Yount, B. (NASA Ames Research Center Moffett Field, CA United States)
Cassell, A. (NASA Ames Research Center Moffett Field, CA United States)
Kruger, C. (NASA Ames Research Center Moffett Field, CA United States)
Brivkalns, C. (NASA Ames Research Center Moffett Field, CA United States)
Makino, A. (NASA Ames Research Center Moffett Field, CA United States)
Duttta, S. (NASA Ames Research Center Moffett Field, CA United States)
Ghassemieh, S. (NASA Ames Research Center Moffett Field, CA United States)
Wu, S. (NASA Ames Research Center Moffett Field, CA United States)
Battazzo, S. (NASA Ames Research Center Moffett Field, CA United States)
Nishioka, O. (NASA Ames Research Center Moffett Field, CA United States)
Venkatapathy, E. (NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
March 9, 2017
Publication Date
March 4, 2017
Subject Category
Launch Vehicles And Launch Operations
Engineering (General)
Report/Patent Number
ARC-E-DAA-TN39728
Meeting Information
Meeting: IEEE Aerospace Conference
Location: Big Sky, MT
Country: United States
Start Date: March 4, 2017
End Date: March 11, 2017
Sponsors: American Inst. of Aeronautics and Astronautics, Institute of Electrical and Electronics Engineers
Funding Number(s)
WBS: WBS 513851
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
mechanical
decelerator
deployable

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