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Thermal Accommodation of Payloads on German Spacelab Mission D1
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English
Abstract
The payloads to be flown on the German Spacelab D1 mission in October 1985 located in the Module are thermally accommodated by a combined air/water cooling system, whilst the experiments on the Unique Support Structure are designed for autonomous operation.
This paper describes the work performed on the thermal system under contract of DFVLR to satisfy the requirements of the experiments and those of the Space Shuttle.
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Schwarz, B. and Hafkemeyer, H., "Thermal Accommodation of Payloads on German Spacelab Mission D1," SAE Technical Paper 851362, 1985, https://doi.org/10.4271/851362.Also In
References
- Hafkemeyer H.P. “PLE-Thermal Mathematical Model Requirements” ERNO Report D1-IN-SP-025-ER
- “Spacelab Payload Accommodation Handbook” Main Volume - Appendix C ESA SLP/2104 June 1982
- Hafkemeyer H.P. “D1 System Thermal Analysis Report” Part 1: D1-ECLS-THM Description/User Guide ERNO Report D1-IN-TN-131-ER
- “MDTSCO Spacelab Long Module ECLS Thermal Model” Description and User Guide MDC-G-9815 A
- Hafkemeyer H.P. “D1 System Thermal Analysis Report” Part 4: D1-AVLF-MM Avionics Loop Air Flow Analysis ERNO Report D1-IN-TN-162-ER
- “MDTSCO Spacelab Avionics Loop Flow Model” Description and User Guide MDC-G-9838 A