Publication | Closed Access
Overview of the ASPIRE Project's Supersonic Flight Tests of a Strengthened DGB Parachute
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Citations
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References
2019
Year
Unknown Venue
Aspire ProjectAeronauticsEngineeringAerospace EngineeringStrengthened Dgb ParachuteAerospace SimulationAerospace TechnologyStrengthened ParachuteAerodynamicsSpace SciencesAspire Instrumentation SuiteAerospace SystemParachute DesignsApplied AerodynamicsSupersonic Flight TestsFlight Validation
The Advanced Supersonic Parachute Inflation Research Experiments (ASPIRE) project is aimed at developing and exercising a capability for testing supersonic parachutes at Mars-relevant conditions. The initial flights for ASPIRE were targeted as a risk-reduction activity for NASA's upcoming Mars2020 mission. For this effort, two candidate Disk-Gap-Band (DGB) parachute designs were tested at Mach number and dynamic pressure conditions relevant to Mars2020. The two parachutes under investigation were a build-to-print version of the DGB used by the Mars Science Laboratory and a strengthened version of this parachute that has the same geometry but differs in materials and construction. The first flight test (SR01) of the build-to-print parachute took place on October 4, 2017, followed by the first test of the strengthened parachute during flight SR02 on March 31, 2018. A second test of the strengthened parachute with a higher target load, SR03, took place on September 7, 2018. During the SR02 test, a Terrier-Black Brant sounding rocket delivered a payload containing the packed 21.5-m parachute, the deployment mortar, and the ASPIRE instrumentation suite to a peak altitude of 54.8 km. As the payload descended back towards the Atlantic Ocean the strengthened parachute was mortar-deployed at a Mach number of 1.97 and a dynamic pressure of 670 Pa, and produced a peak load of 55.8 klbf. During the SR03 flight, the strengthened parachute was deployed from an identical test platform at a Mach number of 1.85 and a dynamic pressure of 932 Pa, and produced a peak force of 67.4 klbf. This paper describes ASPIRE's two sounding rocket flight tests of the strengthened parachute: SR02 and SR03. It provides an overview of flight operations, test conditions, the data acquired during testing, the techniques used for post-flight reconstruction, and the reconstructed performance of the test vehicle and parachute system for each flight.
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