SBIR/STTR Research Award

A First Response Crew Mask for Ammonia, Hydrazine and Combustion Products

Award identifier 9ecbdf96f0fcceff4312e1a2aeccfe26d2dfc0f1457db530bdfc3741dfb91db6Awarding agency National Aeronautics and Space Administration

Award amount

$749,995

Program and phase

SBIR · Phase II

Award year

2014

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
TDA RESEARCH, INC.
Proposal award date
2014-04-23
Contract end date
2016-04-22
UEI
MK5ANJVWVZK7
Solicitation number
Not reported
Topic code
H3.02

Research abstract

The increasing frequency of International Space Station (ISS) egress operations contaminates the spacecraft environment with propellant residues (such as anhydrous hydrazine) and their decomposition by-products, as well as coolants such as ammonia and Freon. NH3 and N2H4 have a 24 hour Spacecraft Maximum Allowable Concentration (SMAC) of 7 ppm and 0.3 ppm, respectively. TDA Research Inc. is developing a new adsorbent that can remove these contaminants to sub ppmv concentrations with high activity and capacity. The sorbent can be integrated as a thin layer into an existing cartridge used in the ISS first response crew mask; the new media will greatly extend the capability to protect against the NH3 and hydrazine for extended duration under high contaminant challenges, without undermining the ability of the cartridge to filter out other combustion by-products. In Phase I, we successfully completed all proof-of-concept demonstrations at the bench-scale elevating the TRL to 3. The new adsorbent can provide over 1,400 minutes of protection when challenged with 50 ppmv NH3 and over 450 hrs with 1 ppmv anhydrous N2H4, even at a bed aspect ratio as low as 0.1 and at gas-solid contact times as low as 0.11 sec. The NH3 and N2H4 capacity of the sorbent exceeds 1.8% wt. and 1.4% wt., respectively, with bed outlet concentrations maintained at less than 40 ppbv. In Phase II, we will continue to optimize the sorbent formulations and scale-up the production. We will design and fabricate full-scale experimental prototype cartridges at TDA to support demonstrations in an environmental chamber using a breathing apparatus. Based on the results, we will design and fabricate high fidelity cartridges based on the flight qualified ISS Fire Recovery Respirator Cartridge and complete high fidelity demonstrations in an environmental chamber to fully demonstrate its capability (non-human testing at TRL 6). These will be provided to NASA for additional testing and demonstrations.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

951 SBIR/STTR records share this UEI (1988–2026). Reported award amounts total $317,960,224. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, Department of Energy, National Aeronautics and Space Administration, Environmental Protection Agency, National Science Foundation, Department of Health and Human Services

Agency intelligence

National Aeronautics and Space Administration

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