NASA SBIR 2019-II Solicitation

Proposal Summary


PROPOSAL NUMBER:
 19-2- A1.04-3055
PHASE 1 CONTRACT NUMBER:
 80NSSC19C0374
SUBTOPIC TITLE:
 Electrified Aircraft Propulsion
PROPOSAL TITLE:
 High Energy Density and High Cycle Life Lithium-Sulfur Battery For Electrified Aircraft Propulsion
SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Giner, Inc.
89 Rumford Avenue
Newton, MA 02466
(781) 529-0500

PRINCIPAL INVESTIGATOR (Name, E-mail, Mail Address, City/State/Zip, Phone)
Castro S.T. Laicer
claicer@ginerinc.com
89 Rumford Avenue
Newton, MA 02466 - 1311
(781) 529-0546

BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Cortney Mittelsteadt Ph.D.
cmittelsteadt@ginerinc.com
89 Rumford Avenue
Newton, MA 02466 - 1311
(781) 529-0529

Estimated Technology Readiness Level (TRL) :
Begin: 3
End: 5
Technical Abstract (Limit 2000 characters, approximately 200 words)

A high cycle life and high energy density rechargeable battery will address an important growing demand for safe, efficient, low-cost, environmentally sustainable air transportation. These advances will enable “thin-haul” aircraft with low-carbon propulsion systems that provide low-cost passenger and package transportation. Advances in electrified aircraft propulsion (EAP) will also introduce a new class of small aircraft with vertical take-off and landing capability for on-demand, urban air taxi and regional commuter service applications. Lithium-sulfur (Li-S) batteries are promising next-generation energy storage devices for NASA EAP program applications because of their high theoretical gravimetric energy density of 2500 Wh/kg, which is up to 5 times higher than today’s commercial lithium-ion batteries. However, their use has been limited by poor cycle life caused in part by the poor stability of Li metal anodes during cycling.

In Phase II, Giner will build on a successful Phase I feasibility demonstration to scale up its novel coating technology for stabilizing Li metal anodes in prototype Li-S pouch cells.

Potential NASA Applications (Limit 1500 characters, approximately 150 words)

The developed technology will enable the use of high energy density Li-S batteries with increased cycle life for various NASA missions and programs such as: EAP applications (urban air mobility, thin haul, and short haul aircraft), EVA applications (life support, communications, power tools, glove heaters, lights and other devices), satellites, and other spacecraft and vehicles such as JUNO and the planned new Mars rover.

Potential Non-NASA Applications (Limit 1500 characters, approximately 150 words)

This technology will enable commercialization of high energy density Li-S batteries with increased cycle life. This improvement will make Li-S batteries more practical for electric vehicle applications. Additional markets include power for unmanned aerial vehicles, aerospace vehicles, military satellites, large-scale grid energy storage, and consumer electronics.

Duration: 24

Form Generated on 05/04/2020 06:26:05