NASA SBIR 2017 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 171 H10.03-9107
SUBTOPIC TITLE: Cryogenic Purge Gas Recovery and Reclamation
PROPOSAL TITLE: H2/He Separation System

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
TDA Research, Inc.
12345 West 52nd Avenue
Wheat Ridge, CO 80033 - 1916
(303) 422-7819

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. Gokhan Alptekin Ph.D.
galptekin@tda.com
12345 West 52nd Avenue
Wheat Ridge, CO 80033 - 1916
(303) 940-2349

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: 2
End: 3

Technology Available (TAV) Subtopics
Cryogenic Purge Gas Recovery and Reclamation 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)
NASA uses an estimated 75 million standard cubic feet of helium (approximately $5M worth) each year for safely purging hydrogen systems before filling and after discharging, and while leak checking, pressurizing lines and blanketing liquid hydrogen storage tanks. Despite its expense, there is no substitute for helium in most of these applications because of its extremely low boiling point and unique chemical inertness. The price of helium is expected to increase as reserves are drawn down. In addition to helium, the high supply costs and limited availability of hydrogen fuel also requires its conservation. While it is not as expensive as helium and is more abundant, the transport of hydrogen is still costly and poses a great environmental risk due its flammability and highly reactive nature. Therefore, an efficient way to separate the He/H2 from NASA?s purge streams and recover both the helium and hydrogen in a pure form is critical to reduce cost of operations and to reduce risks. In Phase I we will synthesize and optimize a new sorbent and develop a process and cycle scheme that will allow us to achieve the target helium and hydrogen purities with low energy consumption.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The main attraction of our research to NASA is to ensure the long-term sustainability of programs that rely on helium gas for system purging, leak checking, and as a blanket gas for liquid H2 tanks. The cost of a single recovery unit that is conservatively capable of reclaiming $950,000 of high-purity helium per year is expected to be less than $2.5 million. Depending on the amount of hydrogen that is mixed with the helium, the hydrogen recovered from purge gases (and boiloff) could be of similar value. NASA?s future launch systems are built around hydrogen-oxygen rockets, and the need for large quantities of helium will therefore continue for decades. TDA?s He-H2 recovery system can be used to capture large and small He-H2 purge and boil-off streams at their source to save money, conserve resources, and improve the environmental sustainability of NASA?s operations.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
There is a real and far larger commercial opportunity for our technology in the chemical and energy industries. There is worldwide interest in storage and pressurization systems for hydrogen as an efficient and clean energy carrier. Air Liquide and Linde are already exploring hydrogen compression using solid-state compressors. Hence, the primary customers would include these technology developers. TDA's technology can be used to recover and purify hydrogen from streams that are currently vented or flared in the oil refining, chemical, ammonia, methanol, chlor-alkali, metallurgical, glass and electronics industries.

The technological readiness level (TRL) will be elevated from 2 to 3 at the end of Phase I. In Phase II we will design, build and test a sub-scale prototype system to demonstrate the feasibility of the concept, thereby elevating the TRL to 4.

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.)
Cryogenic/Fluid Systems
Fluids
Fuels/Propellants
Launch Engine/Booster
Prototyping

Form Generated on 04-19-17 12:59