Performance of Supersonic Parachutes behind Slender BodiesNASA's ASPIRE (Advanced Supersonic Parachute Inflation ResearchExperiments) project is investigating the supersonic deployment, inflation andaerodynamics of full-scale disk-gap-band (DGB) parachutes. The first two flight tests werecarried out in October 2017 and March 2018, while a third test is planned for the fall of 2018. Inthese tests, Mars-relevant conditions are achieved by deploying the parachutes at high altitudesover Earth using a sounding rocket test platform. As a result, the parachute is deployed behind aslender body (roughly 1/6-th the diameter of the capsule that will use this parachute for descentat Mars). Because there is limited flight and experimental data for supersonic DGBs behindslender bodies, the development of the parachute aerodynamic models was informed by CFDsimulations of both the leading body wake and the parachute canopy. This presentation willdescribe the development of the pre-flight parachute aerodynamic models and compare preflightpredictions with the reconstructed performance of the parachute during the flight tests.Specific attention will be paid to the differences in parachute performance behind blunt andslender bodies.
Document ID
20190025129
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Muppidi, Suman (Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
O'Farrell, Clara (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Van Norman, John (Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Clark, Ian (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
May 15, 2019
Publication Date
November 19, 2018
Subject Category
Spacecraft Design, Testing And PerformanceAerodynamics
Report/Patent Number
ARC-E-DAA-TN63360Report Number: ARC-E-DAA-TN63360
Meeting Information
Meeting: American Physical Societyýs Division of Fluid Dynamics (DFD)