NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
MEMS based pumped liquid cooling systems for micro/nano spacecraft thermal controlThe 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.
Document ID
20060031280
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Birur, G. C.
Shakkottai, P.
Sur, T. W
Date Acquired
August 23, 2013
Publication Date
March 13, 2001
Distribution Limits
Public
Copyright
Other
Keywords
Microelectromechanical systems(MEMS) thermal control microspacecraft pumped
liquid cooling system

Available Downloads

There are no available downloads for this record.
No Preview Available