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Study on the Development of a Small ETG for the Korean Launch Vehicle’s Low Orbit Test

Jintae Hong, Kwang-Jae Son, Jong-Bum Kim, Jin-Joo Kim

Nuclear Technology / Volume 206 / Number 8 / August 2020 / Pages 1213-1223

Technical Paper / dx.doi.org/10.1080/00295450.2019.1682899

Received:June 27, 2019
Accepted:October 17, 2019
Published:August 4, 2020

The Korea Aerospace Research Institute is planning to launch a satellite for the Korea launch vehicle’s low orbit test in 2021. An electrically heated thermoelectric generator (ETG) with a mass of 850 g (small ETG) will be one of its selected payloads for this test flight. To assess and assure the design heritage and the reliability of the ETG in the space environment, a small ETG will be tested at the top of the satellite for more than a year. In this study, the design for a small ETG with 10 W(thermal) of heat input was developed through simulations such as heat transfer analysis, modal analysis, thermoelectric analysis, and structural analysis. Then a mock-up was fabricated and basic performance tests were carried out to be ready for the space environment test.