Thermal system verification and model validation for NASA's cryogenic passively cooled james webb space telescope (JWST)

SAE Technical Papers

Volumn , Issue , 2005, Pages

  Cleveland, Paul E ^a   Parrish, Keith A ^b  

^a Energy Solutions International

^b NASA GODDARD SPACE FLIGHT CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CADMIUM ALLOYS; CADMIUM TELLURIDE; COOLING; CRYOGENICS; II-VI SEMICONDUCTORS; INTERPLANETARY FLIGHT; MERCURY AMALGAMS; MERCURY COMPOUNDS; NASA; OBSERVATORIES; SEMICONDUCTOR ALLOYS; SOFTWARE TESTING;

FLIGHT CONFIGURATIONS; JAMES WEBB SPACE TELESCOPE; LOW TEMPERATURES; MERCURY CADMIUM TELLURIDE; MODEL VALIDATION; THERMAL ARCHITECTURE; THERMAL BALANCE TEST; VERIFICATION PLANS;

SPACE TELESCOPES;

EID: 85072426722     PISSN: 01487191     EISSN: 26883627     Source Type: Journal    
DOI: 10.4271/2005-01-3042     Document Type: Conference Paper

References (3)

1. Parrish K., Glazer S., Thomson S., "The Cryogenic Thermal System Design of NASA's James Webb Space Telescope (JWST) Integrated Science Instrument Module (ISIM)" Paper 05ICES-206 presented at the 2005 International Conference on Environmental Systems (ICES) (Rome, Italy-July 11-14, 2005).
2. Donabedian M., "Thermal Control Margins, Risk Estimation, and Lessons Learned," Chapter 19 in Spacecraft Thermal Control Handbook Volume II: Cryogenics, edited by Donabedian M., (The Aerospace Press, El Segundo, California, 2003)
3. General Environmental Verification Specification for STS and ELV Payloads, Subsystems, and Components, Revision A, (GEVS-SE), June 1996, Section 2.6, Thermal.