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Aerodynamic Performance of the 2018 InSight Mars LanderInSight touched down in Elysium Planitia on 26 November 2018, becoming NASA’s eighth successful entry, descent, and landing (EDL) at Mars. InSight was a build-to-print of the successful 2008 Phoenix EDL system, flying a non-spinning, ballistic trajectory with a 70-degree sphere-cone aeroshell (2.65-meter diameter), disk-gap-band parachute, and pulsed terminal descent and landing engines. This work discusses entry aerodynamic performance for InSight up to parachute deployment, including pre-flight aerodynamics predictions and comparisons with post-flight reconstruction, as well as comparisons with the Phoenix reconstruction.
Document ID
20200002812
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Ashley M Korzun
(Langley Research Center Hampton, Virginia, United States)
Robert W Maddock
(Langley Research Center Hampton, Virginia, United States)
Mark Schoenenberger
(Langley Research Center Hampton, Virginia, United States)
Karl T Edquist
(Langley Research Center Hampton, Virginia, United States)
Carlie H Zumwalt
(Langley Research Center Hampton, Virginia, United States)
Christopher Karlgaard
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Date Acquired
April 20, 2020
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NF1676L-33332
Meeting Information
Meeting: AIAA SciTech 2020
Location: Orlando, FL
Country: US
Start Date: January 6, 2020
End Date: January 10, 2020
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 336763.01.04.15
Distribution Limits
Public
Copyright
Public Use Permitted.
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