Metabolic Heat Regenerated Temperature Swing Adsorption for CO2, Thermal and Humidity Control

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$599,999.00
Award Year:
2009
Program:
SBIR
Phase:
Phase II
Contract:
NNX09CB09C
Agency Tracking Number:
074640
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
Paragon Space Development Corporation
3481 E. Michigan Street, Tucson, AZ, 85714
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
837002294
Principal Investigator:
Christine Iacomini
Principal Investigator
(520) 382-4824
ciacomini@paragonsdc.com
Business Contact:
Carole Hammond
Business Official
(520) 382-4814
chammond@paragonsdc.com
Research Institution:
n/a
Abstract
MTSA technology specifically addresses the thermal, CO2 and humidity control challenges faced by Portable Life Support Systems (PLSS) to be used in NASA's Constellation Program. Metabolically-produced CO2 present in the ventilation gas of a PLSS is collected using a CO2-selective adsorbent via temperature swing adsorption. The temperature swing is achieved through cooling to well below metabolic temperatures. The coolant can be water, liquid CO2 (LCO2), or any cryogenic fluid. Water or LCO2 is used as coolant by expanding the liquid to below sublimation temperatures when exposed to low pressure or vacuum environments. Subsequent super heated vapor, as well as additional coolant, is used to further cool the astronaut. The adsorbent is warmed using moist ventilation gas, producing condensation which is recycled at the habitat. The overall objective of the Phase 2 effort is to develop and test in a relevant environment a full-scale lunar PLSS MTSA subassembly Engineering Development Unit (EDU) comprised of a condensing ice heat exchanger (CIHX), a sorbent bed and a sublimation heat exchanger (HX). This will be achieved by developing high fidelity models and designs of the three functions, validated with test data available from previous work. At the completion of the effort, the EDU will have been manufactured and tested. The MTSA subassembly will be at TRL 5 and the EDU can be used for off-nominal operational testing as well as MTSA system integration tests.

* information listed above is at the time of submission.

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