MMOD testing of C-SiC based Rigid External Insulation of the CRV Thermal Protection System

Details MMOD testing of C-SiC based Rigid External Insulation of the CRV Thermal Protection System MMOD testing of C-SiC based Rigid External Insulation of the CRV Thermal Protection System

Jan 2002

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2002iaf..confe.458c&link_type=abstract

IAF abstracts, 34th COSPAR Scientific Assembly, The Second World Space Congress, held 10-19 October, 2002 in Houston, TX, USA.,

Computer Science

Scientific paper

is to provide protection to the vehicle during the reentry, it also has to resist Micro Meteoroids and Orbital Debris (MMOD) aggression during the required 3 years in orbit stay of the CRV. composite panels that are fixed to the metallic airframe. An innovative approach for the thermal protection is to use a Rigid External Insulation composed of a C-SiC panel, an internal light insulation, attachment system and seal directly fixed on the metallic airframe. includes firstly a preliminary TPS design based on CRV specifications, then a comparison of the proposed REI design with the current tile. impacts, generic test articles have been designed and manufactured then exposed to MMOD testing. design of the TPS, the manufacturing of the test items, MMOD testing and results.

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