Radiator heat pump subsystem for the space suit portable life support

C. Silva, Michael Schuller, E. Marotta

Research output: Contribution to journalConference article

Abstract

The study of conceptual designs for a space suit Personal Life Support Subsystem (PLSS) at the Texas Engineering Experiment Station resulted in the recommendation to NASA of an evolution path from the existing PLSS to a long duration, low mass PLSS suitable for Martian missions. The replacement of the water sublimator cooling unit by a radiator-mechanical heat pump subsystem was one of the key technology upgrades for this evolution. The assessment was based on using a carbon radiator and mechanical heat pump. The "Lunar Noon" environment was used for sizing the system. The effect of lunar dust on the radiator and choice of refrigerant fluid were considered. A survey of previous work on high temperature heat pumps was made in order to estimate the maturation time for the heat pump technology. We concluded that a heat pump radiator using water as its cooling fluid was the best alternative.

Original languageEnglish
JournalSAE Technical Papers
DOIs
Publication statusPublished - 1 Jan 2009
EventInternational Conference on Environmental Systems, ICES 2009 - Savannah, GA, United States
Duration: 12 Jul 200912 Jul 2009

Fingerprint

Radiators
Pumps
Fluids
Cooling water
Refrigerants
Conceptual design
Dust
NASA
Hot Temperature
Cooling
Carbon
Water
Experiments
Temperature

ASJC Scopus subject areas

  • Automotive Engineering
  • Safety, Risk, Reliability and Quality
  • Pollution
  • Industrial and Manufacturing Engineering

Cite this

Radiator heat pump subsystem for the space suit portable life support. / Silva, C.; Schuller, Michael; Marotta, E.

In: SAE Technical Papers, 01.01.2009.

Research output: Contribution to journalConference article

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