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Vacuum-RegenerableTrace Contaminant Control for Exploration Portable Life Support System

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: 80NSSC21C0533
Agency Tracking Number: 205200
Amount: $749,251.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: H4
Solicitation Number: SBIR_20_P2
Solicitation Year: 2020
Award Year: 2021
Award Start Date (Proposal Award Date): 2021-07-28
Award End Date (Contract End Date): 2023-07-27
Small Business Information
410 Sackett Point Road
North Haven, CT 06473-3106
United States
DUNS: 178154456
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Christian Junaedi
 (203) 287-3700
Business Contact
 Rebecca O'Connor
Title: roconnor
Phone: (203) 287-3700
Research Institution

Precision Combustion, Inc. (PCI) proposes a compact, vacuum-regenerable sorbent bed for effectively removing a broad range of trace contaminants, meeting topic performance requirements, which can be integrated with the Exploration Portable Life Support System (xPLSS) CO2/H2O removal system. Both the primary trace contaminants (ammonia, CO, formaldehyde, and methyl mercaptan) as well as other species that threaten to exceed the 7-day Spacecraft Maximum Allowable Concentration (SMAC) levels during an EVA were addressed via sub-scale testing in Phase I. These sorbents with different properties were combined in the modular Trace Contaminant Control (TCC) bed, tailored to the requirements and in suitable proportion. Our approach is based on PCIrsquo;s proven sorbent nanomaterials that have high surface area on a structured support, enabling a compact, low pressure drop, and vacuum-regenerable TCC device. In Phase I, all objectives and proposed tasks were successfully completed to demonstrate proof-of-concept of these vacuum-regenerable sorbent materials and sorbent module for a compact, efficient TCC. This offers the potential for real-time, in-suit sorbent regeneration, reduced logistical burden associated with bed replacement or thermal regeneration, and further volume and weight reduction of the TCC packaging. At the end of Phase I, a modular, compact, low pressure drop, and durable integrated TCC design approach was identified. In this proposed follow-on Phase II, TCC hardware prototypes will be developed, demonstrated, and delivered to a NASA laboratory for further evaluation, performance validation, and possible integration with the xPLSS hardware design. This effort would be valuable to NASA as it would address the current xPLSS technology gap and increase mission capability/durability/extensibility while at the same time increasing the TRL of the novel vacuum regenerable TCC sorbents.

* Information listed above is at the time of submission. *

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