MLI Impact Phenomenology Observed on the HST Bay 5 MLI Panel

[摘要] Multi-layer insulation (MLI) blankets covering the Hubble Space Telescope (HST) electronics bays were removed during HST Servicing Mission 4 and returned to Earth for analysis. The NASA Orbital Debris Program Office obtained HST Bay 5, 8, and 10 MLI blankets to characterize impact features and develop a flux estimate based on those features. This paper reports on the impact feature phenomenology observed during imaging campaigns in 2011 and 2018. Earlier conventions of measuring impacted features by recording the largest diameter to determine impacting particle size do not provide the best subsequent estimation of the impacting particle size. Instead of an impacted feature as a smooth-edged through-hole, a ‘petaling’ phenomenon along with multiple-layering composition in impacted features has been observed in both hypervelocity testing and in the Bay 5 MLI. A new methodology of characterization techniques used during research and analysis of the HST MLI is presented, which will provide greater understanding and a more accurate estimation of impacting particles and their parameters.

[发布日期] 2019-12-09

[学科分类] 机械工程学

[关键词] MULTILAYER INSULATION;HUBBLE SPACE TELESCOPE;PHENOMENOLOGY;SPACE DEBRIS;IMPACT DAMAGE;IMPACT TOLERANCES;CHARACTERIZATION