Thermal Model Correlation and Validation of a 6U Nanosatellite with Multiple Payloads

Author:

Kim Ji-Seok,Kim Hae-DongORCID

Funder

Korea Aerospace Research Institute

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Reference11 articles.

1. MIL-STD-1540E/SMC-TR-06-11 (2006) Test requirements for launch, upper-stage, and space vehicles, TR-2004(8583)-1 REV.A, The Aerospace Corporation, CA

2. Kang SJ, Oh HW (2016) On-orbit thermal design and validation of 1U standardized CubeSat of STEP Cube Lab. Int J Aerosp Eng 26:1–17. https://doi.org/10.1155/2016/4213189

3. James PM, Bret L, Thomas NW, Chloe D (2018) CubeSat on-orbit temperature comparison to thermal-balance-tuned-model predictions. J Thermophys Heat Transfer 32(1):237–255. https://doi.org/10.2514/1.T55169

4. Fennell TW Jr. (2020) Thermal management design of a 6U CubeSat with a high-power additive manufacturing payload using analytical modeling with experimental validation. Master Dissertation, Florida Institute of Technology, Melbourne, Florida

5. Song YB, Park SY, Lee SW (2021) Development of spacecraft formation flying system for SNIPE mission using four Nanosats. AIAA SciTech Forum. https://doi.org/10.2514/6.2021-0426

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