Simulation of orbital debris impact on the Space Shuttle wing leading edge

Author:

Fahrenthold Eric P.,Hernandez Roque J.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Ocean Engineering,Safety, Risk, Reliability and Quality,Aerospace Engineering,Automotive Engineering,Civil and Structural Engineering

Reference19 articles.

1. Hypervelocity impact testing of transparent spacecraft materials;Burt;Int J Imp Eng,2003

2. Report of the Columbia Accident Investigation Board. Vol. 1, DC, Washington: Government Printing Office; 2003.

3. Penetration equations for thermal protection materials;Christiansen;Int J Imp Eng,1997

4. Lyons L, Christiansen EL, Kerr JH. Hypervelocity impact testing of RCC composites. Report JSC 23898, NASA Johnson Space Center, May 1998.

5. Simulation of hypervelocity impact effects on reinforced carbon–carbon;Park;AIAA Journal of Spacecraft and Rockets,2006

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