Reduction of flight hardware outgassing after integration under a less stringent requirement

Proceedings of SPIE - The International Society for Optical Engineering

Volumn 2864, Issue , 1996, Pages 235-245

  Hughes, David W ^a   Rosecrans, Glenn P ^a   Triolo, Jack J ^a   Hansen, Patricia A ^b  

^a Swales and Associates Inc   (United States)

^b NASA GODDARD SPACE FLIGHT CENTER   (United States)

Author keywords

Adsorber; Bakeout; FGS; HST; Outgassing

Indexed keywords

DEGASSING; OPTICAL SYSTEMS; STRAY LIGHT;

ADSORBERS; BAKE-OUT; BAKEOUT TEMPERATURES; CONTAMINATION REDUCTION; FINE GUIDANCE SENSORS; HUBBLE SPACE TELESCOPES; SERVICING MISSIONS; STRINGENT REQUIREMENT;

CONTAMINATION;

EID: 5344270495     PISSN: 0277786X     EISSN: 1996756X     Source Type: Conference Proceeding    
DOI: 10.1117/12.258315     Document Type: Conference Paper

References (4)

1. Hedgeland, R. J., Hansen, P. A., and Hughes, D. W., "An Integrated Approach for Contamination Control and Verification for the Hubble Space Telescope First Servicing Mission", SPIE Optical Systems Contamination: Effects, Measurement, Control IV, paper no. 2261-03, July 1994
2. Lee, A. L. and Fong, M. C, "HST HUB Contamination Analysis Updated for COSTAR Sources", LMSC Internal Memorandum, FS&S 790, 31 October 1993
3. Kays, R and Mahone, W; "A prototype test system to measure the mass loss of condensable outgassed products in an isothermal vacuum", AIAA/ASME 4th Joint Thermophysics and Heat Transfer Conference, 1986
4. Barengoltz, J., Moore, S., Soules, D., and Voecks, G.; The Wide Field Planetary Camera 2 Molecular Adsorber. JPL Publication 94-001, 15 Jan 1994