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Development of Engineering Qualification Model of a Small ETG for a Launch Environmental Test

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

Nuclear Technology / Volume 207 / Number 6 / June 2021 / Pages 790-800

Technical Paper / dx.doi.org/10.1080/00295450.2020.1832417

Received:July 23, 2020
Accepted:October 1, 2020
Published:May 28, 2021

According to the development plan for the Korea Space Launch Vehicle, a performance verification satellite will be installed in the launch vehicle in 2021. In addition, three payloads, including a small electrically heated thermoelectric generator (ETG), will be developed and installed in the satellite. In particular, a small ETG has been developed by the Korea Atomic Energy Research Institute for the purpose of evaluating the characteristics of the ETG in the space environment prior to the development of a radioisotope thermoelectric generator for lunar missions. In this study, shock and vibration tests were carried out to check whether the ETG can endure the launch environment of the spacecraft. In addition, a thermal cycle test and a thermal vacuum test were conducted to check whether the ETG maintains its performance, even at drastic temperature changes, which can be applied to the ETG in space. Finally, a periodic performance test was carried out to measure the degradation level of the small ETG.