Estimate of the influence of thermophysical parameter deviations on spacecraft's thermal regime
Heading:
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.
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Keywords: telemetry information, thermal control system, thermophysical properties |
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).