SBIR/STTR Research Award

Modular Advanced Cryocooler Electronics

Award identifier 63475d7763b8868b64fa50c8fa5e9b855d7064f1cbef34e330139ab265f98006Awarding agency Department of Defense · Air Force

Award amount

$869,567

Program and phase

SBIR · Phase II

Award year

2013

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
IRIS TECHNOLOGY CORPORATION
Proposal award date
2013-06-14
Contract end date
2015-01-14
UEI
FZNZJD7228P5
Solicitation number
2005.1
Topic code
MDA05-017

Research abstract

ABSTRACT: The proposed effort for the Modular Advanced Cryocooler Electronics (MACE) is to increase the Technology Readiness Level (TRL) of the current MACE technology to support near term insertion into a spaceborne platform. MACE will be used to drive and control the Raytheon Stirling / Pulse Tube Two-Stage (RSP2) Cryocooler. The RSP2 is of great interest to the Department of Defense because it is the only spaceflight cryocooler available that can provide appreciable refrigeration (>400 mW) at 10K. MACE is unique from other cryocooler electronics in that it is architected to support a wide range of cryocoolers. In addition to driving and controlling the above-described 10K cryocooler from Raytheon, MACE is equally applicable to the 35K Raytheon variant of RSP2. With straightforward changes to the control firmware, MACE also supports comparably sized cryocoolers from other vendors. BENEFIT: The immediate benefit to USAF and the Department of Defense is that MACE will be the first spaceflight design cryocooler electronics for the Raytheon RSP2 Cryocooler, which is the best performing 10K Cryocooler available. This program will yield a high fidelity brassboard with a part-for-part upgrade path to a spaceflight design, greatly reducing the risk for technology insertion. More generally, MACE will provide the space cryocooler user community with a control electronics platform that can support virtually any cryocooler need. MACE"s 600W drive capacity envelopes the practical power range of interest. MACE provides simultaneous temperature, vibration, and piston position control. Incorporation of a low frequency input ripple filter simplifies insertion by enabling direct connection to the primary spacecraft bus.

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

26 SBIR/STTR records share this UEI (2006–2023). Reported award amounts total $12,441,596. 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

Agency intelligence

Department of Defense

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