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Adaptive Deployable Entry Placement Technology (ADEPT) Development for Small Sat Class Venus MissionsThe Adaptable, Deployable Entry and Placement Technology (ADEPT) is a novel approach for entry vehicle design. Similar to an umbrella, it is stowed during launch and deployed prior to entry. ADEPT employs a high performance, 3-D woven, carbon fabric to serve as the primary surface of the mechanically deployed system. The successful ADEPT sounding rocket flight test matured the 1-meter Class ADEPT in the areas of deployment and structural integrity, and provided aerodynamic flight characteristics of the ADEPT open-back configuration from Mach 3 to Mach 0.3. Aerocapture uses the aerodynamic drag from a single hyperbolic atmospheric pass to provide the delta-V needed for orbit insertion. Studies suggest that, compared to propulsive orbit insertion, aerocapture could increase delivered payload by 70 percent at Venus. Drag modulation aerocapture, which shows promise of being simpler and more cost-effective than the more-often studied lift modulation methods, uses in-flight transformations of an entry vehicle's drag area to control the amount of deceleration produced during an atmospheric pass. In single-event drag modulation, a drag device is jettisoned after the appropriate deceleration. ADEPT, due to its unique ability to fold and unfold, is being considered for this SmallSat class payload mission applications.
Document ID
20190011701
Acquisition Source
Ames Research Center
Document Type
Poster
Authors
Cassell, Alan M.
(NASA Ames Research Center Moffett Field, CA, United States)
Wercinski, Paul F.
(NASA Ames Research Center Moffett Field, CA, United States)
Venkatapathy, Ethiraj
(NASA Ames Research Center Moffett Field, CA, United States)
Aftosmis, Michael J.
(NASA Ames Research Center Moffett Field, CA, United States)
Wilder, Michael C.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
May 8, 2019
Publication Date
November 6, 2018
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
ARC-E-DAA-TN62552
Report Number: ARC-E-DAA-TN62552
Meeting Information
Meeting: Venus Exploration Analysis Group (VEXAG) Meeting
Location: Laurel, MD
Country: United States
Start Date: November 6, 2018
End Date: November 8, 2018
Sponsors: Johns Hopkins Univ., Lunar and Planetary Institute (LPI), NASA Goddard Space Flight Center
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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