NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Flight Performance of the Inflatable Reentry Vehicle Experiment 3The Inflatable Reentry Vehicle Experiment 3 (IRVE-3) launched July 23, 2012, from NASA Wallops Flight Facility (WFF) on a Black Brant XI suborbital sounding rocket and successfully performed its mission, demonstrating the survivability of a hypersonic inflatable aerodynamic decelerator (HIAD) in the reentry heating environment and also illustrating the effect of an offset center of gravity on the HIAD's lift-to-drag ratio. IRVE-3 was a follow-on to 2009's IRVE-II mission, which demonstrated exo-atmospheric inflation, reentry survivability - without significant heating - and the aerodynamic stability of a HIAD down to subsonic flight conditions. NASA Langley Research Center is leading the development of HIAD technology for use on future interplanetary and Earth reentry missions.
Document ID
20140000147
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Dillman, Robert
(NASA Langley Research Center Hampton, VA, United States)
DiNonno, John
(NASA Langley Research Center Hampton, VA, United States)
Bodkin, Richard
(NASA Langley Research Center Hampton, VA, United States)
Gsell, Valerie
(NASA Wallops Flight Facility Wallops Island, VA, United States)
Miller, Nathanael
(NASA Langley Research Center Hampton, VA, United States)
Olds, Aaron
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Bruce, Walter
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
January 13, 2014
Publication Date
June 17, 2013
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NF1676L-16379
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
Funding Number(s)
WBS: WBS 432938.08.01.07.02
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available