Vulnerability of spacecraft electronics boxes to hypervelocity impacts

International Astronautical Federation - 56th International Astronautical Congress 2005

Volumn 4, Issue , 2005, Pages 2637-2647

  Putzar, Robin ^a   Schäfer, Frank ^a   Stokes, Hedley ^b   Chant, Richard ^b   Lambert, Michel ^c  

^a FRAUNHOFER INSTITUTE FOR HIGH SPEED DYNAMICS   (Germany)

^b QINETIQ   (United Kingdom)

^c EUROPEAN SPACE AGENCY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

CONTRACTS; ELECTRONIC EQUIPMENT; FIELD PROGRAMMABLE GATE ARRAYS (FPGA); IMPACT TESTING; PRINTED CIRCUIT BOARDS; RANDOM ACCESS STORAGE;

ALUMINIUM CASING; ELECTRONICS BOXES; MULTI-LAYER INSULATION (MLI); SANDWICH PANEL (SP);

SPACECRAFT;

EID: 34250828651     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. Putzar, Robin; Schäfer, Frank; Romberg, Oliver; Lambert, Michel: Vulnerability of shielded fuel pipes and heat pipes to hypervelocity impacts, Proceedings of the 4th European Conference on Space Debris, 2005.
2. Frost, Cynthia L.; Rodriguez, Pedro L: AXAF hypervelocity impact test results, Proceedings of the 2nd European Conference on Space Debris, 1997.
3. Lambert, Michel; Schäfer, Frank; Geyer, Tobias: Impact damage on sandwich panels and multi-layer insulation, Int. J. Impact Engng, 26, 369-380, 2001.
4. Dahl, Kim V.; Cour-Palais, Burt G.: Standardization of impact damage classification and measurements for metallic targets, to be published, 1991.