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Hybrid Anode for Electrified Aircraft Propulsion

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: 80NSSC19C0543
Agency Tracking Number: 193203
Amount: $124,991.00
Phase: Phase I
Program: STTR
Solicitation Topic Code: T15
Solicitation Number: STTR_19_P1
Timeline
Solicitation Year: 2019
Award Year: 2019
Award Start Date (Proposal Award Date): 2019-08-19
Award End Date (Contract End Date): 2020-09-18
Small Business Information
510 Earl Boulevard
Miamisburg, OH 45342-6411
United States
DUNS: 130020209
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Brian Henslee
 (937) 320-1877
 hensleeb@crgrp.com
Business Contact
 Jackie Luce
Phone: (937) 320-1877
Email: lucejm@crgrp.com
Research Institution
 University of Maryland
 
3112 Lee Building, 7809 Regents Drive
College Park, MD 20742-5141
United States

 Federally Funded R&D Center (FFRDC)
Abstract

Electrified Aircraft Propulsion (EAP) research is part of NASA effort to improve aircraft fuel efficiency, emissions, and noise levels. New secondary battery chemistries are required to meet the 500 ndash; 700 Wh/kg cell level specific energy needs of UAM, all-electric helicopters and regional passenger aircraft. The cycle life, currently at asymp; 1500 ndash; 3000 cycles, also needs substantial improvement. Safety is another important consideration: battery fires, not uncommon in electric cars, are unacceptable in aircraft.Cornerstone Research Group proposes to develop battery cells based on new anode and electrolyte chemistry to meet the NASArsquo;s operational needs for high specific energy, long-lasting and safe EAP energy storage.

* Information listed above is at the time of submission. *

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