Comparison between Solar Simulation and Infrared Technique for Thermal Balance Test
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Comparison between Solar Simulation and Infrared Technique for Thermal Balance Test

Authors: Tao Tao, Wang Jing, Cao Zhisong, Liu Yi, Qie Dianfu

Abstract:

The precision of heat flux simulation influences the temperature field and test aberration for TB test and also reflects the test level for spacecraft development. This paper describes TB tests for a small satellite using solar simulator, electric heaters, calrod heaters to evaluate the difference of the three methods. Under the same boundary condition, calrod heaters cases were about 6oC higher than solar simulator cases and electric heaters cases for non-external-heat-flux cases (extreme low temperature cases). While calrod heaters cases and electric heaters cases were 5~7oC and 2~3oC lower than solar simulator cases respectively for high temperature cases. The results show that the solar simulator is better than calrod heaters for its better collimation, non-homogeneity and stability.

Keywords: solar simulation, infrared simulation, TB test, TMM

Digital Object Identifier (DOI): doi.org/10.5281/zenodo.1328544

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References:


[1] Richard Eddy, "Design and Construction of the JPL SS15B Solar simulator," JPL internal document, 1968.
[2] P.W. Brinkman, "Main Characteristics of The Large Space Simulator (LSS) at ESA/ESTEC," 13th Space Simulation Conference.
[3] F. Muller-Stute, "Test Support Hardware for the ESTEC Large Space Simulator (LSS)".
[4] R. Satish etc., "Preparations and performance of Large Space Simulation Chamber (LSSC) during INSAT-2E solar simulation thermal balance and thermal vacuum performance tests," 21th Space Simulation Conference.
[5] Kurt A. Beckel, "The two axis Motion Simulator for the Large Space Simulator at ESTEC," 15th Space Simulation Conference.
[6] Dr. Holm Frey etc., "Possible Modifications of ESA-s Large Space Simulator to Produce a 3-Meter Diameter Beam of 10 Solar Constant," 2002.
[7] William. N. Breeden ð¿ etc., "Solar Thermal Vacuum Testing of The MARS Global Surveyor Spacecraft," 19th Space Simulation Conference.
[8] William N. Breeden III, "Thermal Vacuum Testing of the Mars Surveyor Program and Stardust Spacecraft," 20th Space Simulation Conference.
[9] Jacqueline C. Lyra, "The Mars Pathfinder System Level Solar Thermal Vacuum Test," 1997.
[10] E. Sacchi, "An Overview of the Thermal Verification and Testing of Integral and Artemis Satellites," 30th ICES.
[11] S. G. Price, "Polar Platform Service Module Thermal Balance Testing and Correlation".
[12] H.R.D. Jones and N.C. Rowe, "Validation of infra-red test techniques using solar simulation," in Proc. AIAA/AHS/ASEE Aerospace Design Conference, Irvine, CA, 1993.
[13] Pietro Giordano, Giuseppe Andrina, Luca Cane, Bruno Panella, "Mercury Thermal Testing with Use of IR Techniques," 2003.
[14] Giuseppe Andrina, Luca Cane, Bruno Panella, "Solar Simulation v/s IR Techniques Applicability to Mercury/Bepicolombo Probes System Thermal Test," in Proc. 4th International symposium on Environement Test for Space Programmes, Liege Belgium, 2001.