Hypervelocity impact on carbon fibre reinforced plastic (CFRP)/aluminium honeycomb at normal and oblique angles

European Space Agency, (Special Publication) ESA SP

Volumn , Issue 393, 1997, Pages 429-434

  Taylor, Emma A ^a   Herbert, Mark K ^a,b   Kay, Laurie ^a  

^a UNIVERSITY OF KENT   (United Kingdom)

^b AIRBUS DEFENCE AND SPACE   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 5244227807     PISSN: 03796566     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article

References (7)

1. Gehring, J.W. (1970), Chapter IX : Engineering considerations, in High Velocity Impact Phenomena, Academic Press, New York, ed. R. Kinslow.
2. Taylor, E.A., Herbert, M.K., Gardner, D.J., Griffiths, A.D., Kay, L., Thomson, R. and Burchell, M.J., Hypervelocity Impact on Carbon Fibre Reinforced Plastic (CFRP) / Aluminium Honeycomb: Risk Assessment for Low Earth Orbiting Spacecraft, Submitted to Proceedings of the Institution of Mechanical Engineers Part G : Journal of Aerospace Engineering.
3. Lambert, M. (1996), Hypervelocity impacts and damage laws, presented at COSPAR '96, Birmingham, 14-21 July 1996. Accepted for publication in Adv. Space Res.
4. Christiansen, E.L. (1992), Performance equations for advanced orbital debris shields, AIAA 92-1462, presented at the AIAA Space Programs and Technologies Conference, March 24-27 1992, Huntsville, AL.
5. Drolshagen, G. and Borde, J. (1992), ESABASE Debris-Meteoroid/Debris Impact Analysis Technical Description, ESA ESTEC, ESABASE-GD-01/1, Noordwijk, Netherlands.
6. Christiansen, E.L. (1990), Investigation of hypervelocity impact damage to space station truss tubes, Int. J. Impact Engng., Vol. 10, pp. 125-133.
7. Terrillon, F., Warren, H.R. and Yelle, M.J. (1991), Orbital debris shielding design of the Radarsat spacecraft, IAF-91-283, 42nd International Astronautical Congress, 5-11 October 1991, Montreal, Canada.