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Advanced, Long-Life Cryocooler Technology for Zero-Boil-Off Cryogen Storage

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX08CB71P
Agency Tracking Number: 074171
Amount: $99,958.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: X9.01
Solicitation Number: N/A
Timeline
Solicitation Year: 2007
Award Year: 2008
Award Start Date (Proposal Award Date): 2008-02-06
Award End Date (Contract End Date): 2008-08-05
Small Business Information
P.O. Box 71
Hanover, NH 03755-3116
United States
DUNS: 072021041
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Mark Zagarola
 Principal Investigator
 (603) 640-2360
 mvz@creare.com
Business Contact
 James Barry
Title: President
Phone: (604) 640-2487
Email: contractsmgr@creare.com
Research Institution
N/A
Abstract

Long-life, high-capacity cryocoolers are a critical need for future space systems utilizing stored cryogens. The cooling requirements for planetary and extraterrestrial exploration missions, Crew Exploration Vehicles, extended-life orbital transfer vehicles, and space depots will range from 10 to 50 W at temperatures between 20 and 120 K. Turbo-Brayton cryocoolers are ideal for these systems because they are lightweight, compact and very efficient at high cooling loads, in addition to their inherent attributes of high reliability; negligible vibration; long, maintenance-free lifetimes; and flexibility in integrating with spacecraft systems and instruments. To date, space-borne turbo-Brayton technology has been developed for low cooling loads. During the proposed program, Creare will develop an advanced, high efficiency turbine optimized for a high-capacity cryocooler. The advanced turbine will enable a landmark reduction in cryocooler input power and overall cooling system mass. In Phase I, we will define the requirements for a particular mission class, develop the conceptual design of a multistage cryocooler to meet these requirements, develop the preliminary design of the advanced turbine and perform proof-of-concept tests. During Phase II, we will fabricate the turbine and demonstrate its performance at prototypical operating conditions.

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

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