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Results for “cooling system thermal control microspacecraft”

Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.

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NASA NTRS2000

MEMS based pumped liquid cooling systems for micro/nano spacecraft thermal control

The electronic and other payload power densities in future micro/nano spacecraft are expected to exceed 25 Watts/cm(sup 2) and require advanced thermal control concepts and technologies to keep their payload within allowable temperature limits. This paper presents background on the need for pumped liquid cooling systems for future micro/nano spacecraft and results from this ongoing experimental investigation.

cooling system thermal control microspacecraft↗

NASA NTRS2001

MEMS based pumped liquid cooling systems for micro/nano spacecraft thermal control

The objective is to develop MEMS based pumped liquid cooling system for removing over 20 W/cm squared from high power density microelectronics and science payloads considered for future micro/nano sciencecraft.

Microelectromechanical systems(MEMS) thermal contr↗

NASA NTRS2001

Micro/nano spacecraft thermal control using MEMS-based pumped liquid cooling system

This paper presents background on the need for pumped liquid cooling systems for future micro/nano spacecraft and results from this ongoing numerical and experimental investigation.

microchannel microspacecraft thermal control elctr↗