NASA STTR 2016 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 16-2 T6.04-9773
PHASE 1 CONTRACT NUMBER: NNX16CA52P
RESEARCH SUBTOPIC TITLE: Closed-Loop Living System for Deep-Space ECLSS with Immediate Applications for a Sustainable Planet
PROPOSAL TITLE: Highly Efficient Closed-Loop CO2 Removal System for Deep-Space ECLSS

SMALL BUSINESS CONCERN (SBC): RESEARCH INSTITUTION (RI):
NAME: TDA Research, Inc. NAME: University of Puerto Rico - Mayaguez
STREET: 12345 West 52nd Avenue STREET: Call Box 9000
CITY: Wheat Ridge CITY: Mayaguez
STATE/ZIP: CO  80033 - 1916 STATE/ZIP: PR  00681 - 9000
PHONE: (303) 940-2347 PHONE: (787) 832-4040

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. Ambalavanan Jayaraman Ph.D.
ajayaraman@tda.com
12345 West 52nd Avenue
Wheat Ridge, CO 80033 - 1916
(303) 940-5391

CORPORATE/BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Mr. John D. Wright
jdwright@tda.com
12345 West 52nd Avenue
Wheat Ridge, CO 80033 - 1916
(303) 940-2300

Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 3
End: 5

Technology Available (TAV) Subtopics
Closed-Loop Living System for Deep-Space ECLSS with Immediate Applications for a Sustainable Planet is a Technology Available (TAV) subtopic that includes NASA Intellectual Property (IP). Do you plan to use the NASA IP under the award?
No

TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)

TDA Research Inc.(TDA) in collaboration with University of Puerto Rico – Mayaguez (UPRM is proposing to develop a highly efficient CO2 removal system based on UPRM proprietary strontium exchanged silico-alumino-phosphate (Sr-SAPO-34) sorbent for closed loop space craft cabin air re-vitalization during deep space missions.

 

In the Phase I work, we successfully completed bench-scale proof-of-concept demonstrations, elevating the TRL to 3. In Phase II, we will further optimize the sorbent and scale-up its production using advanced manufacturing techniques such as continuous microwave synthesis.  We will carry out multiple adsorption/desorption cycles to demonstrate the sorbent's cycle life (>500).  We will develop a CFD model to optimize the cyclic operation of the sorbent system and carry out a detailed engineering assessment of the full-scale system.  Finally, we will design and fabricate a sub-scale prototype to fully demonstrate the technology under simulated spacecraft cabin atmospheres (TRL-5); this unit will be sent to NASA for further testing and evaluation.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The main attraction of our research to NASA is its ability to provide a lightweight, compact and energy efficient CO2 removal system for closed-loop space craft cabin air re-vitalization during deep space missions.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
This system will also find use on earth for removing CO2 from confined spaces such as large buildings, aircrafts, and submarines to reduce the energy use of next generation life support and air conditioning systems. The sorbent developed is also applicable to a wide variety of industrial processes, which require CO2 removal (i.e., CO2 capture from flue gas, biogas, natural gas, etc.) and sorbent enhanced water-gas-shift reaction in hydrogen manufacturing.

TECHNOLOGY TAXONOMY MAPPING (NASA's technology taxonomy has been developed by the SBIR-STTR program to disseminate awareness of proposed and awarded R/R&D in the agency. It is a listing of over 100 technologies, sorted into broad categories, of interest to NASA.)
Essential Life Resources (Oxygen, Water, Nutrients)
Prototyping
Sources (Renewable, Nonrenewable)

Form Generated on 04-26-18 12:32