SBIR-STTR Award

Advanced Multipollutant Trace Contaminant Sorbents for the Exploration Portable Life Support System
Award last edited on: 2/24/2021

Sponsored Program
SBIR
Awarding Agency
NASA : JSC
Total Award Amount
$873,547
Award Phase
2
Solicitation Topic Code
H4.01
Principal Investigator
Marek A Wojtowicz

Company Information

Advanced Fuel Research Inc (AKA: AFR)

87 Church Street
East Hartford, CT 06108
   (860) 528-9806
   info@afrinc.com
   www.afrinc.com
Location: Single
Congr. District: 01
County: Hartford

Phase I

Contract Number: 80NSSC20C0553
Start Date: 8/27/2020    Completed: 3/1/2021
Phase I year
2020
Phase I Amount
$124,976
This proposal addresses the fabrication and testing of structured (monolithic), carbon-based multipollutant trace-contaminant (TC) sorbents for the space suit used in Extravehicular Activities (EVAs). The proposed innovations are: (1) multipollutant trace-contaminant control; (2) thin-walled, structured carbon TC sorbents fabricated using three-dimensional (3D) printing; and (3) the patented low-temperature oxidation step used for the treatment of carbon sorbents. The overall objective is to develop a multipollutant trace-contaminant removal system that is rapidly vacuum-regenerable and that possesses substantial weight, size, and power-requirement advantages with respect to the current state of the art. The Phase 1 objectives are: (1) to demonstrate the effectiveness of monolithic carbon sorbents with respect to ammonia and formaldehyde removal at concentrations much lower than currently demonstrated and tested, i.e. << 20 ppm ammonia and << 3 ppm formaldehyde; (the proposed target is the 7-day Spacecraft Maximum Allowable Concentrations, SMAC); (2) to evaluate the monolithic carbon sorbents with respect to multipollutant TC control, including carbon monoxide and methyl mercaptan; to define a path to sorbent improvements, if needed; and (3) to deliver a sorbent prototype to NASA for further sub-scale testing. This will be accomplished in three tasks: (1) Sorbent Fabrication and Characterization; (2) Sorbent Testing; and (3) Product Assessment. Potential NASA Applications (Limit 1500 characters, approximately 150 words) The main application of the proposed technology would be in spacecraft life-support systems, mainly in extravehicular activities (space suit), but after modifications also in cabin-air revitalization. Potential Non-NASA Applications (Limit 1500 characters, approximately 150 words) The developed technology may find applications in air-revitalization on board US Navy submarines, in commercial and military aircraft, in the future air-conditioning systems for green buildings, and in advanced scuba-diving systems.

Phase II

Contract Number: 80NSSC21C0508
Start Date: 9/3/2021    Completed: 9/2/2023
Phase II year
2021
Phase II Amount
$748,571
This proposal addresses the fabrication and testing of structured (monolithic), carbon-based multipollutant trace-contaminant (TC) sorbents for the space-suit Exploration Portable Life Support System (xPLSS) used in Extravehicular Activities (EVAs). The proposed innovations: (1) multipollutant trace-contaminant control; (2) thin-walled, structured carbon TC sorbents fabricated using three-dimensional (3D) printing; and (3) the patented low-temperature oxidation step used for the treatment of carbon sorbents. The overall objective: to develop a multipollutant trace-contaminant removal system that is rapidly vacuum-regenerable and that possesses substantial weight, size, and power-requirement advantages with respect to the current state of the art. The Phase 1 project successfully demonstrated the effectiveness of monolithic carbon sorbents derived from 3D-printed PEEK polymer with respect to ammonia, formaldehyde, and methyl mercaptan removal at concentrations close to 7-day Spacecraft Maximum Allowable Concentration (SMAC) limits. The sorbent monoliths were also evaluated with respect to carbon-monoxide control, and a path to multipollutant TC control was defined for future R&D. The Phase 2 objectives: (1) to optimize sorbent properties and performance; (2) to design, construct, test, and deliver to NASA two full-scale TC sorbent prototypes; (3) to integrate the full-scale TC Control System (TCCS) with the xPLSS design, and particularly with the Rapid-Cycle Amine (RCA) swing bed for CO2 control. This work will be accomplished in five tasks: (1) Sorbent Development and Optimization; (2) Subscale Sorbent Testing; (3) Full-Scale Prototype Development; (4) Full-Scale Prototype Integration with xPLSS/RCA and Testing; and (5) System Evaluation. The main focus will be full-scale TCCS development and its integration with xPLSS/RCA (Tasks 3 and 4). Potential NASA Applications (Limit 1500 characters, approximately 150 words): The main application of the proposed technology would be in spacecraft life-support systems, mainly in extravehicular activities (space suit), but after modifications also in cabin-air revitalization. Potential Non-NASA Applications (Limit 1500 characters, approximately 150 words): The developed technology may find applications in air-revitalization on board US Navy submarines, in commercial and military aircraft, in the future air-conditioning systems for green buildings, and in advanced scuba-diving systems. Duration: 24