Estimate of the influence of thermophysical parameter deviations on spacecraft's thermal regime

Heading: 
Space Energy, Power and Propulsion
1Petrov, Yu.V, 2Rassamakin, BM, 1Taranova, TA, 3Khoroshylov, VS
1Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine
2National Technical University of Ukraine “Igor Sikorsky Kyiv Polytechnic Institute”, Kyiv, Ukraine
3Yangel Yuzhnoye State Design Office, Dnipro, Ukraine
Kosm. nauka tehnol. 2006, 12 ;(1):018-022
https://doi.org/10.15407/knit2006.01.018
Publication Language: Russian
Abstract: 
The necessity of accurate information on actual values of thermophysical properties for the SC with passive thermal control system is substantiated. On the basis of the telemetry information from the temperature sensors of the AUOS-SM-KF SC, the degradation of black enamel AK-512 is analyzed using inverse-scattering method as well as effective thermal conductivity of honeycomb panel and embedded heat-pipes is estimated.
Keywords: telemetry information, thermal control system, thermophysical properties
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References: 
1. Rassamakin B. M., Tarasov G. B., Khairnasov, et al. Modeling and Analysis of On-Earth and Flight Tests of Honeycomb Panels Containing Heat Pipes on Board of "AMPOS CM-KF" Spacecraft. In: Kosmicheskaja tehnika. Raketnoe vooruzhenie: Nauchno-tehn. sb., 264—276 (GKB Juzhnoe, Dnepropetrovsk, 2004) [in Russian].
2. Silverman E. M. Space environmental effects on spacecraft: LEO materials selection guide. Progress Rep., TRW Space and Electronics Group, Redondo Beach, California, Contract NASI-19291, April 1993 through March 1995, 1099—10101 (1995).