SBIR/STTR Research Award

Lightweight Recuperator for Electrified Aircraft Propulsion

Award identifier 822baa3f274ba124c5dd7f86249ae152eb3141fce3a3a2b10bfde57837c35673Awarding agency National Aeronautics and Space Administration

Award amount

$749,982

Program and phase

SBIR · Phase II

Award year

2021

Explore This Research Award in CaptureIQ

Research the technology, evaluate the recipient and agency, identify related opportunities, and explore potential follow-on work with CaptureIQ.

Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
Micro Cooling Concepts, Inc
Proposal award date
2021-07-14
Contract end date
2023-07-13
UEI
UYXJFFNQ6V71
Solicitation number
SBIR_20_P2
Topic code
A1

Research abstract

Electrified Aircraft Propulsion (EAP) is a growing NASA technology effort that could enable new configurations of aircraft. With the potential to transform the transportation and services markets, vehicle classes of interest include single-aisle, thin/short haul, and urban air mobility. These vehicle concepts rely on hybrid electric systems to provide propulsive power through the use of a turbo-generator combined with electrical energy storage. For turbo-generators/range-extenders utilized in regional EAP concepts, small lightweight turboshaft engines are an excellent choice due to their maturity and availability. However, at small power scales, gas turbines are less efficient. This can be addressed using a recuperator to inject waste heat from the turbine back into the thermodynamic cycle upstream of the combustor.nbsp;Micro Cooling Concepts (MC2) has developed technologies for fabricating extremely compact metallic heat exchangers with high heat transfer while reducing size and weight by 2-3X, using the printed circuit heat exchanger (PCHX) approach.nbsp;Using additive manufacturing to create heat exchangers with finer scale and higher aspect ratio features can magnify the advantages of MC2rsquo;s existing technology, resulting in recuperators with minimal weight, volume, and pressure losses.nbsp;Analysis shows that the 3D-printed hybrid laminate recuperators provide reductions in volumes and weight of 4.4X and 7.7X, respectively, compared to conventional recuperators.nbsp;These weight reductions translate directly into shorter fuel payback times and opportunities to increase payload or range. The program will consist of recuperator design studies, fabrication studies, fabrication and testing of sub-scale test articles, and full-scale prototype fabrication and testing at engine relevant conditions. This effort supports the NASA goal ofnbsp;reducing the mass and increasing the efficiency of heat acquisition and rejection componentsnbsp;and advancing technologies for more electric aircraft.

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.

Research funding history

22 SBIR/STTR records share this UEI (2003–2024). Reported award amounts total $7,661,842. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: National Aeronautics and Space Administration, Department of Defense, Department of Energy

Agency intelligence

National Aeronautics and Space Administration

Back to SBIR/STTR Research Awards

Don't take our word for it. Ask AI about RFPCapture.

See what leading AI assistants have to say about RFPCapture and CaptureIQ.

Gemini opens without a prefilled question. The question is copied to your clipboard when the button works. You can also copy it here:

What is RFPCapture.com and its CaptureIQ platform from Smart Logic AI? How does it help federal contractors discover opportunities, evaluate bid/no-bid decisions, research government contracts, and prepare proposals? How does it compare with other federal capture platforms? Use independent sources where available.