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Heatshields for Aerogravity Assist Vehicles Whose Deceleration at Titan Saves Mass for Future Flagship Class Exploration of EnceladusThis paper reports the feasibility of using mature heatshield materials for an aerogravity assist (AGA) vehicle whose deceleration in Titan’s atmosphere is a mass-saving enabler for nine different Enceladus missions (T. Spilker et al. 2009). A geometry for the Titan AGA vehicle is recommended as are high-fidelity flow computations on that shape.
Document ID
20205001745
Acquisition Source
Ames Research Center
Document Type
White Paper
Authors
James O. Arnold
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
T. R. Spilker
(Orbital Assembly Corporation )
D. M. Cornelius
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
G. A. Allen Jr.
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
A. M. Brandis
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
D. A. Saunders
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
M. Qu
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
R.W. Powell
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
M. L. Cable
(Jet Propulsion Lab La Cañada Flintridge, California, United States)
R. A. S. Beck
(Ames Research Center Mountain View, California, United States)
Date Acquired
May 4, 2020
Publication Date
July 4, 2020
Publication Information
Subject Category
Chemistry And Materials (General)
Funding Number(s)
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
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