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IRVE-3 Post-Flight ReconstructionThe Inflatable Re-entry Vehicle Experiment 3 (IRVE-3) was conducted from the NASA Wallops Flight Facility on July 23, 2012. Launched on a Black Brant XI sounding rocket, the IRVE-3 research vehicle achieved an apogee of 469 km, deployed and inflated a Hypersonic Inflatable Aerodynamic Decelerator (HIAD), re-entered the Earth's atmosphere at Mach 10 and achieved a peak deceleration of 20 g's before descending to splashdown roughly 20 minutes after launch. This paper presents the filtering methodology and results associated with the development of the Best Estimated Trajectory of the IRVE-3 flight test. The reconstructed trajectory is compared against project requirements and pre-flight predictions of entry state, aerodynamics, HIAD flexibility, and attitude control system performance.
Document ID
20130013398
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Olds, Aaron D.
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Beck, Roger
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Bose, David
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
White, Joseph
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Edquist, Karl
(NASA Langley Research Center Hampton, VA, United States)
Hollis, Brian
(NASA Langley Research Center Hampton, VA, United States)
Lindell, Michael
(NASA Langley Research Center Hampton, VA, United States)
Cheatwood, F. N.
(NASA Langley Research Center Hampton, VA, United States)
Gsell, Valerie
(Orbital Sciences Corp. Wallops Island, VA, United States)
Bowden, Ernest
(Orbital Sciences Corp. Wallops Island, VA, United States)
Date Acquired
August 27, 2013
Publication Date
March 25, 2013
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA Paper 1514242
Meeting Information
Meeting: 22nd AIAA Aerodynamic Decelerator Systems Technology Conference
Location: Daytona Beach, FL
Country: United States
Start Date: March 25, 2013
End Date: March 28, 2013
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 677714.05.01.07
Distribution Limits
Public
Copyright
Public Use Permitted.
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