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Advanced Supersonic Parachute Inflation Research Experiment Preflight Trajectory Modeling and Postflight ReconstructionThe Advanced Supersonic Parachute Inflation Research and Experiments (ASPIRE) was a series of sounding rocket flights aimed at understanding the dynamics of supersonic parachutes that are used for Mars robotic applications. The 2012 Mars Science Laboratory (MSL) had a successful deployment of a supersonic parachute, but based on post-flight analysis of parachute margins, the ASPIRE project was created as a risk-reduction program to improve quantification of these margins and qualify a supersonic parachute for Mars 2020, the follow-on mission to MSL. The first sounding rocket (SR01) flight of ASPIRE occurred near Wallops Island, Virginia on Oct. 4, 2017 and demonstrated the successful deployment and inflation of a MSL build-to-print parachute in flight conditions similar to the 2012 MSL mission. The ASPIRE SR02 and SR03 were successful follow-on flights on Mar. 31, 2018 and Sep. 7, 2018 that demonstrated the new, strengthened supersonic parachute designed for the Mars 2020 project. The SR02 and SR03 parachuteswere targeted to 100% and 140% of the expected flight limit load for Mars 2020 to confirm new margins expected from the strengthened parachute. Prior to all flights, a multi-body flight dynamics simulation was developed to predict the parachute dynamics and was used, in conjunction with other tools, to target Mars-relevant flight conditions. After each flight, the on-board data were used to reconstruct the flight trajectory and to validate the pre-flight dynamics simulation. Post-flight analysis showed that all three tests achieved their targeted conditions and pre-flight modeling bounded the key performance metrics for the parachute. This paper describes the flight mechanics simulation, post-flight reconstruction, and the reconciliation process used to validate the flight models.
Document ID
20205001100
Acquisition Source
Langley Research Center
Document Type
Accepted Manuscript (Version with final changes)
Authors
Soumyo Dutta
(Langley Research Center Hampton, Virginia, United States)
Christopher D. Karlgaard
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Jake A. Tynis
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Clara O'Farrell
(Jet Propulsion Lab La Cañada Flintridge, California, United States)
Bryan S. Sonneveldt
(Jet Propulsion Lab La Cañada Flintridge, California, United States)
Eric M. Queen
(Langley Research Center Hampton, Virginia, United States)
Angela L. Bowes
(Langley Research Center Hampton, Virginia, United States)
Emily A. Leylek
(Jet Propulsion Lab La Cañada Flintridge, California, United States)
Mark C. Ivanov
(Jet Propulsion Lab La Cañada Flintridge, California, United States)
Date Acquired
April 20, 2020
Publication Date
October 1, 2020
Publication Information
Publication: Journal of Spacecraft and Rockets
Publisher: American Institute of Aeronautics and Astronautics
Volume: 57
Issue: 6
Issue Publication Date: November 1, 2020
ISSN: 0022-4650
e-ISSN: 1533-6794
Subject Category
Spacecraft Design, Testing And Performance
Funding Number(s)
WBS: 971200.02.07.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
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