Fiber optic cable assemblies for space flight II: Thermal and radiation effects

Proceedings of SPIE - The International Society for Optical Engineering

Volumn 3440, Issue , 1998, Pages 37-46

  Ott, Melanie N ^a  

^a NASA GODDARD SPACE FLIGHT CENTER   (United States)

Author keywords

Cable; Cable assemblies; Fiber optic; Jacketing; Multimode; Preconditioning; Radiation effects; Shrinkage; Space flight; Thermal effects

Indexed keywords

RADIATION EFFECTS; SHRINKAGE; SPACE FLIGHT; THERMAL CYCLING; THERMAL EFFECTS;

JACKETING;

OPTICAL CABLES;

EID: 0002021516     PISSN: 0277786X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1117/12.326697     Document Type: Conference Paper

References (4)

1. M. Ott, J. Plante, J. Shaw, M. A. Garrison Darrin "Fiber Optic Cable Assemblies for Space Flight: Issues and Remedies," Paper number 975592 AIAA/SAE World Aviation Congress, Anaheim, CA 1997, pp. 1-7.
2. th Biennial Department of Defense Fiber Optics and Photonics Conference, March 22-24, 1994.
3. E. J. Friebele, "Survivability of Photonic Systems in Space" DoD Fiber Optics Conference, McLean VA, March 24-27, 1992.
4. C. E. Barnes "Technology Assessment: Radiation Hardened Fiber Optic and Optoelectronic Devices and Systems," Report to the Defense Nuclear Agency, April 1992.