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Development and In-orbit Performance of a Thermal Control System for Nickel-Cadmium Batteries Based on Loop Heat Pipes
Technical Paper
2000-01-2456
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
In 1995 TAIS Ltd developed and manufactured a Thermal Control System (TCS) for Nickel-Cadmium Batteries (NCB) based on Loop Heat Pipes (LHP). This TCS was ordered for the Chinese meteorological satellite FY-1C by Shanghai Institute of Spacecraft Engineering.
The paper presents results of comparative analysis for some design features of the TCS, thermal vacuum test results, description of TCS layout for the NCB on board the FY-1 C satellite, test results for TSC after its integration into the satellite and flight telemetry data.
Authors
Citation
Goncharov, K., Golovin, O., Kolesnikov, V., Cong, S. et al., "Development and In-orbit Performance of a Thermal Control System for Nickel-Cadmium Batteries Based on Loop Heat Pipes," SAE Technical Paper 2000-01-2456, 2000, https://doi.org/10.4271/2000-01-2456.Also In
References
- “The Loop Heat Pipe Experiment on board the «GRANAT» Spacecraft” Orlov A.A. Goncharov K.A. Kotliarov Eu.Yu. Tyklina T.A. Ustinov S.N. Maidanik Yu.F. CPL-97 Workshop Noordwijk, The Netherlands May 20-22 1997
- “Loop Heat Pipes in Thermal Control Systems for «OBZOR» Spacecraft” Goncharov K.A. Nikitkin M.N. Golovin O.A. Fershtater Yu.G. Maidanik Yu.E. Piukov S.A. 25 ICES San Diego July 10-13 1995
- “Loop Heat Pipes for Space Mission Mars 96” Goncharov K.A. Kozmine D.E. Smirnov F.Yu. Nikitkin M.N. Fershtater Yu.G. Maidanik Yu.F. International Seminar and Workshop “Heat Pipes, Heat Pumps, Refrigerators” “Dual-Use Technologies” September 12-15 1995 Minsk, Belarus