SBIR/STTR Research Award

An Ultra Low Power Cryo-Refrigerator for Space

Award identifier 509a6fc80979053e49a8665f2db54a5446dde99e744fbd555fbd8f3b1b8f8450Awarding agency National Aeronautics and Space Administration

Award amount

$899,804

Program and phase

SBIR · Phase II

Award year

2012

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
CREARE LLC
Proposal award date
2012-04-30
Contract end date
2014-06-10
UEI
JDKYAKDT4TT6
Solicitation number
Not reported
Topic code
S1.07

Research abstract

Future NASA Space Science Missions will incorporate detectors, sensors, shields, and telescopes that must be cooled to cryogenic temperatures. An enabling technology for these missions is advanced cryocoolers that can provide continuous and distributed cooling with minimal input power. On this program, Creare proposes to develop and demonstrate an innovative cryocooler that produces refrigeration at temperatures of 30 to 70 K and rejects heat at a temperature of 150 to 210 K with extremely high efficiency. The heat rejected can be absorbed by an upper stage cryocooler or rejected to space through a small cryo-radiator. The overall mass of the cryocooler, cryo-radiator and electronics is nominally 6 kg, the area of the cryo-radiator is 0.8 m2 and the input power is significantly less than current state-of-the-art cryocoolers. The electronics utilize parts that are tolerant to 300 kRad total ionizing dose. In addition, the cryocooler technology is extremely reliable and scalable, and produces no perceptible vibration. The key innovation is a cryogenic compressor which has heritage to the cryogenic circulator developed by Creare and operated on the Hubble Space Telescope for 6.5 years. On the Phase I project, we optimized the cryocooler design for a particular mission class and predicted the performance of the cryocooler using a combination of analyses and component-level test data. On the Phase II project, we will build and test a demonstration cryocooler and cryo-radiator. The Phase II testing will be structured to achieve a TRL of at least 5, and will include cryogenic performance and launch vibration testing.

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.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

1,365 SBIR/STTR records share this UEI (1983–2026). Reported award amounts total $507,020,394. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Health and Human Services, Department of Energy, Department of Transportation, Department of Commerce

Agency intelligence

National Aeronautics and Space Administration

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