NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Adaptable, Deployable Entry and Placement Technology (ADEPT) for Future Mars MissionsThe concept of a mechanically deploy- able hypersonic decelerator, developed initially for high mass (40 MT) human Mars missions, is currently funded by OCT for technology maturation. The ADEPT (Adaptive, Deployable Entry and Placement Technology) project has broad, game-changing applicability to in situ science missions to Venus, Mars, and the Outer Planets.
Document ID
20160000326
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Wercinski, P. (NASA Ames Research Center Moffett Field, CA United States)
Venkatapathy, E. (NASA Ames Research Center Moffett Field, CA United States)
Gage, P. (NASA Ames Research Center Moffett Field, CA United States)
Prabhu, D. (NASA Ames Research Center Moffett Field, CA United States)
Smith, B. (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)
Allen, G. (NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
January 6, 2016
Publication Date
June 20, 2013
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
ARC-E-DAA-TN9854
Meeting Information
Meeting: International Planetary Probe Workshop (IPPW-10)
Location: San Jose, CA
Country: United States
Start Date: June 17, 2013
End Date: June 21, 2013
Sponsors: San Jose State Univ.
Funding Number(s)
WBS: WBS 985295
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TPS
Mars
Decelerator

Related Records

There are no records associated with this record.
No Preview Available