TECHNICAL PAPERS

In-Orbit Demonstration of Two-Phase Heat Transport Technology: TPX/G557 Development & Pre-Launch Testing

Date Published: 1993-07-01
Paper Number: 932301
DOI: 10.4271/932301

Citation:

Delil, A., Heemskerk, J., Dubois, M., van Oost, S. et al., "In-Orbit Demonstration of Two-Phase Heat Transport Technology: TPX/G557 Development & Pre-Launch Testing," SAE Technical Paper 932301, 1993, doi:10.4271/932301.

Author(s):


A.A.M. Delil - National Aerospace Lab. NLR
J.F. Heemskerk - National Aerospace Lab. NLR
M. Dubois - SABCA
S. van Oost - SABCA
W. Supper - ESA/ESTEC
R. Aceti - ESA/ESTEC

Abstract:

Mechanically and capillary pumped two-phase heat transport systems are currently developed to meet the high power and long transport distance requirements of thermal management systems for future spacecraft. Compared to existing single-phase systems, two-phase loops offer important advantages: reduced overall mass and pumping power consumption, virtually isothermal behaviour, adjustable working temperature, insensitivity to variations in heat load and sink temperature, and high flexibility with respect to the location of heat sources within the loop.

File Size: 1107K

Product Status: In Stock

See papers presented at International Conference On Environmental Systems, July 1993, Colorado Springs, CO, USA, Session: International Conference On Environmental Systems

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