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  • Man/System Technology and Life Support  (2)
  • 2015-2019  (2)
  • 1965-1969
  • 1915-1919
  • 1
    Publication Date: 2019-07-25
    Description: The Carbon Dioxide Removal and Compression System (CRCS) is designed to perform both the Carbon Dioxide(CO2) removal and compress CO2 for further processing. The CRCS was designed as a lower power requirement option to the one currently being used on the International Space Station (ISS). This paper describes the final design, fabrication, assembly, and testing of the integrated CRCS. Initial results indicated that the spiral heaters used did not yield uniform heating within both the adsorption and compression beds. In addition, the heaters for the compression bed were insufficient and an additional HVAC jacket was employed to provide heat to the bed.
    Keywords: Man/System Technology and Life Support
    Type: ICES-2016-027 , ARC-E-DAA-TN31675 , International Conference on Environmental Systems; Jul 10, 2016 - Jul 17, 2016; Viena; Austria
    Format: application/pdf
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  • 2
    Publication Date: 2019-11-30
    Description: Long-duration space missions will eventually require a fresh food supply to supplement crew diets, which means growing crops in space. The Passive Orbital Nutrient Delivery System (PONDS) is a new plant growth approach that contains both an area for a contained substrate and a reservoir for water and/or plant nutrient solutions. Ground studies have shown that the system facilitates both reliable water delivery to seeds for germination (e.g., while avoiding overwatering), and transport of water from the reservoir for improved plant growth while providing nutrients and oxygen to the root zone. In ground prototypes a capillary mat wicking material passively links the water/nutrient solution reservoir to a removable rooting module containing a substrate adapted to support plant growth. Oxygen permeable membranes are incorporated into both the reservoir walls and the rooting modules, bringing in oxygen from outside of the system into the reservoir and then into the rooting modules where the plant roots proliferate. Water is delivered from the reservoir to the substrate contained within the rooting module through the use of wicking material inserted into the plant growth substrate both from the bottom and from the sides of the rooting module. The capillary mat material is intrinsically hydrophilic and continuously wicks water to the substrate throughout the plant growth interval. The system is therefore self-watering in terms of supplying water to the root zone encompassed within the rooting module on demand. At the top, a hydrophilic phenolic foam plug surrounds the wick in the seed insertion zone, and both contains the substrate within the rooting module, and facilitates removal of excess moisture from the capillary mat wick before it can encompass seeds prior to germination. This work is supported by NASAs Space Life and Physical Sciences and Research Applications Division (SLPSRAD).
    Keywords: Man/System Technology and Life Support
    Type: KSC-E-DAA-TN69736 , American Society for Gravitational and Space Research (ASGSR) Meeting; Nov 20, 2019 - Nov 23, 2019; Denver, CO; United States
    Format: application/pdf
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