Evaluate fin performance of a space radiator to remove heat generated for outer space application
Heat is generated in spacecrafts due to air-condition system, electronic and electrical equipment, human beings, etc. The heat generated from these sources must be removed in order to maintain the spacecraft at the required temperatures. Heat rejection to outer space is the area of present work wher...
Main Author: | Nor Nashriq Azizi, Abd Shukor |
---|---|
Format: | Undergraduates Project Papers |
Language: | English |
Published: |
2010
|
Subjects: | |
Online Access: | http://umpir.ump.edu.my/id/eprint/1903/ http://umpir.ump.edu.my/id/eprint/1903/ http://umpir.ump.edu.my/id/eprint/1903/1/Nor_Nashriq_Azizi_Abd_Shukor_%28_CD_4946_%29_.pdf |
Similar Items
-
Effect of Tube Spacing, Fin Density and Reynolds Number on Overall Heat Transfer Rate for In-line Configuration
by: Tahseen, Tahseen Ahmad, et al.
Published: (2015) -
Outer space
by: Ford -
Application Of Design Patterns And Space Concepts In
The Development Of Heat Pipes
by: Sharma, Korada Viswanatha
Published: (2010) -
Experimental investigation on effect of fin shape on the thermal-hydraulic performance of compact fin-and- tube heat exchangers
by: P., Moorthy, et al.
Published: (2018) -
State of the art on flow and heat transfer performance of compact fin-and-tube heat exchangers
by: Adam, A. Y., et al.
Published: (2019)