Lightweight Insulation Materials for On-orbit Thermal Management

Award Information
Agency:
Department of Defense
Branch
Missile Defense Agency
Amount:
$99,999.00
Award Year:
2004
Program:
STTR
Phase:
Phase I
Contract:
FA9453-04-M-0329
Award Id:
69791
Agency Tracking Number:
B045-021-0171
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
10814 Preservation View Dr, Suite 205, Tampa, FL, 33626
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
138122069
Principal Investigator:
Akbar Fard
Principal Scientist
(813) 855-8919
ghaneha@hotmail.com
Business Contact:
Akbar Fard
President
(813) 855-8919
ghaneha@hotmail.com
Research Institute:
Tuskegee University
Hassan Mahfuz
101 James Center
Tuskegee, AL, 36088
(334) 727-8985
Nonprofit college or university
Abstract
Advanced Materials Technology, Inc responds to the DoD needs to develop an innovative robust thermal insulation technology to insulate cryogenic temperature-sensitive space systems and components. Sensitive cryogenic structures and their subsystems need to be protected from direct solar heating, earth's albedo, and internal heating. The Current state-of-art insulation technology is totally based on Multi Layer Insulation (MLI) Blankets. However, they suffer from many drawbacks including being extremely labor intensive and on-orbit durability issues. We propose to develop a robust capable thermal blanket technology that will be space qualified, lightweight, produce no outgassing, and have extremely low thermal conductivity. Our technology will enable the STSS optical track telescope and the SBL to minimize power consumption while maintaining critical temperature control of key components without exceeding launch vehicle lift capabilities. The proposed program will focus on developing new multifunctional polyimide foam materials for on-orbit thermal management, which will be capable of retaining structural integrity while accommodating large operating temperatures ranging from cryogenic (-250 C) to elevated (350 C) temperatures conditions. Once the feasibility of the proposed concept is demonstrated in Phase I, we shall scale-up this concept in a Phase II program to meet DoD requirements.

* information listed above is at the time of submission.

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