Low-velocity projectile impact on spacecraft

Acta Astronautica

Volumn 47, Issue 10, 2000, Pages 763-770

  Yasaka, Tetsuo ^a   Hanada, Toshiya ^a   Hirayama, Hiroshi ^a  

^a KYUSHU UNIVERSITY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

HONEYCOMB STRUCTURES; PROJECTILES; RISK ASSESSMENT; STRUCTURAL ANALYSIS; STRUCTURAL PANELS;

HYPERVELOCITY IMPACTS; LOW-VELOCITY PROJECTILE IMPACTS;

SPACECRAFT;

EID: 0034320803     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0094-5765(00)00127-2     Document Type: Article

References (9)

1. McKnight, D. S. and Brechin, C., Debris creation via hypervelocity impact. AIAA Paper 90-0084, January 1990.
2. Bess, T. D., Size distribution of fragment debris produced by simulated meteoroid impact on spacecraft wall. NASA SP-379, 1975.
3. Nebolsine, P. R., Lord, G. W. and Legner, H. H., Debris Characterization Final Report, PSI-TR-399, 1983.
4. Johnson, N. L., History and consequences of on-orbit break-ups. Advances in Space Research, 1985, 5(2), 11-19.
5. Kessler D. J., Orbital debris issues. Advances in Space Research, 1985, 5(2), 3-10.
6. Su, S. -Y. and Kessler, D., Contribution of explosion and future collision fragments to the orbital debris environment. Advances in Space Research, 1985, 5(2), 25-34.
7. Chobotov, V., Spencer D., Schmitt, D., Gupta, T., Hopkins, W. and Knapp, D., Dynamics of debris motion and the collision hazard to spacecraft resulting from an orbital breakup, SD-TR-88-96, 1988.
8. McKnight, D. S., Determination of breakup initial conditions. Journal of Spacecraft, 1991, 28, 470-477.
9. Su, Shin-Yi., The velocity distribution of collisional fragments and its effect on future space debris environment. Advances in Space Research, 1990, 10, 389-392.