Thermal Stability Testing of Two-Phase Thermal Control Hardware for the Surface Water Ocean Topography Mission
Date
2016–07-10
Authors
Journal Title
Journal ISSN
Volume Title
Publisher
46th International Conference on Environmental Systems
Abstract
The thermal architecture of the proposed Surface Water Ocean Topography (SWOT) mission would utilize loop heat pipes (LHPs) and constant conductance heat pipes (CCHPs) to transport waste heat (> 1 kW) from the instrument electronics to the radiator. The main thermal design risk is the ability to maintain a temporal stability of <0.05°C/min in a low earth orbit environment. The stringent thermal requirements are part of the overall error budget needed to meet the primary mission science goals. A testbed was developed to simulate flight-like loads and environments in order to validate the thermal subsystem could meet the temporal stability requirements.
Description
United States
NASA JPL
202
ICES202: Satellite, Payload, and Instrument Thermal Control
Vienna, Austria
Ruwan P. Somawardhana, Jet Propulsion Laboratory/California Institute of Technology, USA
The 46th International Conference on Environmental Systems was held in Vienna, Austria, USA on 10 July 2016 through 14 July 2016.
NASA JPL
202
ICES202: Satellite, Payload, and Instrument Thermal Control
Vienna, Austria
Ruwan P. Somawardhana, Jet Propulsion Laboratory/California Institute of Technology, USA
The 46th International Conference on Environmental Systems was held in Vienna, Austria, USA on 10 July 2016 through 14 July 2016.
Keywords
loop heat pipe, constant conductance heat pipe, SWOT, stability, testing, testbed