Hybrid Heat Pipes for High Heat Flux Spacecraft Thermal Control

Award Information
Agency:
National Aeronautics and Space Administration
Amount:
$99,986.00
Program:
SBIR
Contract:
NNX11CH33P
Solitcitation Year:
2010
Solicitation Number:
N/A
Branch:
N/A
Award Year:
2011
Phase:
Phase I
Agency Tracking Number:
105982
Solicitation Topic Code:
S3.02
Small Business Information
Advanced Cooling Technologies, Inc.
1046 New Holland Ave., Lancaster, PA, 17601-5606
Hubzone Owned:
N
Woman Owned:
N
Socially and Economically Disadvantaged:
N
Duns:
126288336
Principal Investigator
 William Anderson
 Principal Investigator
 (717) 295-6061
 bill.anderson@1-ACT.com
Business Contact
 Jon Zuo
Title: President
Phone: (717) 295-6058
Email: jon.zuo@1-ACT.com
Research Institution
 Stub
Abstract
Grooved aluminum/ammonia Constant Conductance Heat Pipes (CCHPs) are the standard for thermal control in zero-gravity. Unfortunately, they are limited in terms of their heat flux capability, approximately 5W/cm2. Incident heat flux for laser diode applications is on the order of 5-10W/cm2, although this is expected to increase towards 50W/cm2. This is a severe limitation for axial groove (CCHP) as well as loop heat pipes (LHP). Standard CCHPs are also not suitable for Lunar and Martian Landers and Rovers, since they can only operate with a very small adverse elevation, on the order of 0.10 inch. Landers can have tilts of±20<SUP>o</SUP>, while rovers can have tilts of±45<SUP>o</SUP>. As a result, a wick with a higher heat flux capability and pumping capability is required. This program will develop heat pipes with both 1) Sintered wicks, and 2) Hybrid grooved and sintered wicks. Heat pipes with both wick designs will be capable of operating at heat fluxes in the ten's of watts per cm2, and in Lunar or Martian environments at large slopes against gravity. An all-sintered wick will be used when the entire heat pipe must be able to operate against gravity, while a hybrid wick will be used when the condensers will always be gravity aided on the planetary surface.

* information listed above is at the time of submission.

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