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Space-Flight Assessment of a Small-Scale Collins Type Cryocooler Concept

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: F29601-02-C-0155
Agency Tracking Number: 021NM-1570
Amount: $100,000.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: N/A
Solicitation Number: N/A
Timeline
Solicitation Year: N/A
Award Year: 2002
Award Start Date (Proposal Award Date): N/A
Award End Date (Contract End Date): N/A
Small Business Information
176 Waltham Street
Watertown, MA 02472
United States
DUNS: 070615646
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Joseph Gerstmann
 R&D Manager
 (617) 926-6700
 joegers@aol.com
Business Contact
 Andrew Vasilakis
Title: President
Phone: (617) 926-6700
Email: andyv@amtimail.com
Research Institution
N/A
Abstract

"A compact, reliable, efficient and inexpensive cryocooler requiring less than 1kW of power for 2W of cooling at 10Kelvin is being developed and will be demonstrated. This performance is at least twice as efficient as the best current state-of-the-art forsmall low-temperature cryocoolers. The proposed technical approach, whose feasibility has been confirmed, is to apply the advantageous features of large-scale cryogenic refrigerators to compact and reliable small-scale systems by implementing a novelthermodynamic cycle in a mechanically innovative machine. Size, cost and complexity are reduced in the proposed concept by employing a modular design whereby each stage is of identical construction (except for length), and where the heat exchanger andexpander are constructed as an integral unit. The expanders are of extremely simple floating piston construction that requires no seals or mechanical power transmission devices to extract power from the cold expander. Piston motion is controlled byelectro-mechanically actuated "smart" valves that require no mechanical valve linkages or mechanical timing mechanisms. This further reduces system complexity, improves reliability, and eliminates thermal leakage paths. Expander power is dissipated inthe warm end of the expander by throttling gas to and from the compressor suction and discharge, and a reservoir volume. The proposed cryocooler is intended for use by Very Long Wavelength Infrare

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

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