The feasibility study of the thermal control system for medium size or large size satellites was conducted to investigate the capabilities and specifications of devices such as cold plates, a radiator, a mechanical pump, and so on. In the first step of the system development demonstration, the cold plate was selected to investigate the performance among these devices. In this paper, the system concept of the advanced single-phase fluid loop and the evaluation by numerical analysis and experiments are described.
System Studies of Advanced Single-Phase Fluid Loop with Honeycomb-Cored Cold Plate
Sae Technical Papers
International Conference On Environmental Systems ; 1999
1999-07-12
Conference paper
English
System Studies of Advanced Single-Phase Fluid Loop with Honeycomb-Cored Cold Plate
| British Library Conference Proceedings | 1999
| Engineering Index Backfile | 1957
Tradeoffs in Honeycomb Cored Designs
| Emerald Group Publishing | 1988
An Experimental Study of Heat Transfer Characteristics for Honeycomb-cored Coldplate (1st Report)
| British Library Conference Proceedings | 1998
Spacecraft single-phase fluid loop heat dissipation system
| European Patent Office | 2023