RCS-based ballistic limit curves for non-spherical projectiles impacting dual-wall spacecraft systems

Author:

Schonberg W.P.,Williamsen J.E.

Publisher

Elsevier BV

Subject

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

Reference13 articles.

1. Ballistic limit equations for spacecraft shielding;Christiansen;Int J Impact Eng,2001

2. Morrison RH. Investigation of projectile shape effects in hypervelocity impact of a double-sheet structure. NASA TN D-6944 1972.

3. Piekutowski AJ. Hypervelocity impact of non-spherical projectiles: observations and lessons learned from impact tests. In: Fair H, editor. Proceedings of the hypervelocity shielding workshop. Institute of Advanced Technology: Texas; March 1998.

4. Ballistic limit curves for non-spherical projectiles impacting dual-wall systems;Hu;Int J Impact Eng,2003

5. Kessler D, et al. A computer-based orbital debris environment model for spacecraft design and observation in low-earth orbit. NASA report TM-104825, November 1996.

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