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Nano-ADEPT Aeroloads Wind Tunnel TestAnalysis completed since the test suggests that all test objectives were met– This claim will be verified in the coming weeks as the data is examined further– Final disposition of test objective success will be documented in a final reportsubmitted to NASA stakeholders (early August 2015)– Expect conference paper in early 2016• Data products and observations made during testing will be used to refinecomputational models of Nano-ADEPT• Carbon fabric relaxed from its pre-test state during the test– System-level tolerance for relaxation will be driven by destination-specific andmission-specific aerothermal and aerodynamic requirements• Bonus experiment of asymmetric shape demonstrates that an asymmetricdeployable blunt body can be used to generate measureable lift– With a strut actuation system and a robust GN&C algorithm, this effect could beused to steer a blunt body at hypersonic speeds to aid precision landing
Document ID
20160001281
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Smith, Brandon
(NASA Ames Research Center Moffett Field, CA United States)
Cassell, A.
(NASA Ames Research Center Moffett Field, CA United States)
Yount, B.
(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)
Zarchi, K.
(NASA Ames Research Center Moffett Field, CA United States)
McDaniel, R.
(NASA Ames Research Center Moffett Field, CA United States)
Venkatapathy, E.
(NASA Ames Research Center Moffett Field, CA United States)
Swanson, G.
(ERC, Inc. Moffett Field, CA, United States)
Date Acquired
January 29, 2016
Publication Date
June 15, 2015
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
ARC-E-DAA-TN24270
Meeting Information
Meeting: International Planetary Probe Workshop (IPPW-12)
Location: Cologne
Country: Germany
Start Date: June 15, 2015
End Date: June 19, 2015
Sponsors: Deutsche Forschungsanstalt fuer Luft- und Raumfahrt, European Space Agency, NASA Headquarters, Jet Propulsion Lab., California Inst. of Tech.
Funding Number(s)
WBS: WBS 985295.01.02.01
CONTRACT_GRANT: NNA10DE12C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
atmospheric entry
system engineering
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