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To assure mission success of the Solar Probe Plus (SPP) spacecraft, defined by achieving its final mission orbit with a perihelion distance of less than 10 solar radii, it is necessary to define the dust hypervelocity impact (HVI) protection levels provided by its Multi-Layer Insulation (MLI)/thermal blankets with a reliability that is on par with that available for metallic Whipple shields. Recently, we presented an experimentally validated approach being developed at the Johns Hopkins University Applied Physics Laboratory ...
Published by: IEEE Aerospace Conference Proceedings Published on:
Aerospace vehicles; Aluminum; Ballistics; Coremaking; Dust; Honeycomb structures; Interplanetary flight; Orbits; Particle size; Particle size analysis; Sandwich structures; Sensitivity analysis; Shielding; Parker Engineering