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ASPIRE Aerodynamic Models and Flight PerformanceThe Advanced Supersonic Parachute Inflation Research Experiments (ASPIRE) project was launched in 2016 to develop a capability for testing supersonic parachutes at Mars-relevant conditions. Three parachute tests successfully tested two candidate parachute designs and qualified a parachute for NASA’s Mars 2020 mission (that successfully delivered Perseverance rover to the surface of Mars in Feb 2021). To achieve Mars-relevant densities, these parachutes were deployed at targeted conditions at high altitudes over Earth, launched via sounding rockets. ASPIRE Flight Tests provided valuable data on parachute inflation, forces, and aerodynamic behavior. Design of the flight tests depended on flight mechanics simulations which in turn required aerodynamic models for the payload, and the parachute. Computational Fluid Dynamics (CFD) was used to generate these models pre-flight and they are compared against the flight data after the tests. This talk will go over some aspects of the test design, development of pre-flight models, and comparison with flight test data.
Document ID
20210023511
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Suman Muppidi
(Ames Research Center Mountain View, California, United States)
Clara O'Farrell
(Jet Propulsion Lab La Cañada Flintridge, California, United States)
John W Van Norman
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Ian G Clark
(Jet Propulsion Lab La Cañada Flintridge, California, United States)
Date Acquired
October 27, 2021
Subject Category
Aerodynamics
Meeting Information
Meeting: University Seminar
Location: Southampton
Country: GB
Start Date: November 3, 2021
End Date: November 3, 2021
Sponsors: University of Southampton
Funding Number(s)
CONTRACT_GRANT: NNA15BB15C
CONTRACT_GRANT: 80NM0018D0004P00002
CONTRACT_GRANT: 80LARC17C0003
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Flight Test
Supersonic Parachute
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