Self Deploying Nitinol LHP Radiator for Small Spacecraft

Award Information
Agency:
National Aeronautics and Space Administration
Amount:
$99,937.00
Program:
SBIR
Contract:
NNX09CD65P
Solitcitation Year:
2008
Solicitation Number:
N/A
Branch:
N/A
Award Year:
2009
Phase:
Phase I
Agency Tracking Number:
084291
Solicitation Topic Code:
S3.02
Small Business Information
Thermacore, Inc.
780 Eden Road, Lancaster, PA, 17601-4275
Hubzone Owned:
N
Woman Owned:
N
Socially and Economically Disadvantaged:
N
Duns:
055625685
Principal Investigator
 Alfred Phillips
 Principal Investigator
 (717) 519-3137
 a.l.phillips@thermacore.com
Business Contact
 Nelson Gernert
Title: V.P. Engineering & Technology
Phone: (717) 519-5819
Email: n.j.gernert@thermacore.com
Research Institution
N/A
Abstract
Loop heat pipes are commonly used for heat rejection radiators above a few hundred watts. The LHP condener tubing is embedded in composite panels which are manually deployed. By making the LHP condenser tubing out of shape memory alloy tubing, the radiator becomes self deploying and self contained. It will passively deploy when the payload components begin producing significant heat. This not only eliminates the deployment mechanisms and controls, but also provides more flexible stowing arrangement for the radiators. Very small satellites and spacecraft can now have deployable radiators.

* information listed above is at the time of submission.

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