Space station JEM design implementation and testing for orbital debris protection

International Journal of Impact Engineering

Volumn 20, Issue 6-10, 1997, Pages 723-732

  Shiraki, Kuniaki ^a   Terada, Fumio ^a   Harada, Masayuki ^a  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

DESIGN; ENGINEERING; SHIELDING; SPACE DEBRIS; SPACE FLIGHT; TESTING;

JAPANESE EXPERIMENT MODULE;

SPACE STATIONS;

EID: 0031356267     PISSN: 0734743X     EISSN: None     Source Type: Journal    
DOI: 10.1016/s0734-743x(97)87458-1     Document Type: Article

References (4)

1. K. Tasaki, H. Hashimoto and K. Shiraki, Shielding Considerations for the Japanese Experiment Module. AIAA Conference, Baltimore, April (1990).
2. K. Shiraki, T. Itoh, N. Satoh and Y. Shirai, The Results of Hypervelocity Impact Tests. Journal of the Japan Society for Aeronautical and Space Sciences, Vol. 44(512), September (1996).
3. E. L. Christiansen, J. L. Crews, J. E. Williamsen, J. H. Robinson and A. M. Nolen, Enhanced Meteoroid and Orbital Debris Shielding. Int. J. Impact Engng. Vol. 17, PP. 217-228, (1995).
4. J. H. Tillotson, Metallic Equations of State for Hypervelocity Impact, General Atomic Division of General Dynamics, GA-3216, July (1962).