科技报告详细信息
ASPIRE Aerodynamic Models and Flight Performance
Muppidi, Suman ; O'Farrell, Clara ; Van Norman, John W ; Clark, Ian G
关键词: PARACHUTES;    FLIGHT TESTS;    MARS EXPLORATION;    FLIGHT CHARACTERISTICS;    PAYLOADS;    DEPLOYMENT;    TRAJECTORY MEASUREMENT;    DRAG;   
RP-ID  :  ARC-E-DAA-TN62947
学科分类:航空航天科学
美国|英语
来源: NASA Technical Reports Server
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【 摘 要 】
NASA's Advanced Supersonic Parachute Inflation Research Experiments (ASPIRE) project was established to test full-scale supersonic parachutes at Mars-relevant conditions, as a risk-reduction activity for NASA's upcomingMars2020 mission. Deployment and inflation of Disk-Gap-Band (DGB) parachutes were examined at Mach number and dynamic pressure conditions relevant to Mars2020, using a sounding rocket platform. The flight tests examined two parachutes: a build-to-print version of the parachute 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 built-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. Over the sequence of the three tests, the parachute was exposed to increasing aerodynamic loads with the peak load during SR03 being significantly larger than is expected during a Martian descent. All three tests were successful: the parachute deployment and inflation occurred at the intended conditions, the measurement systems performed as designed and provided the data, and the parachutes survived the aerodynamic loads they were exposed to. The flight tests yielded valuable data on parachute forces and high-speed imagery of the deployment and inflation process.
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