SBIR-STTR Award

Spacecraft Thermal Control Management Using Electrochromics
Award last edited on: 4/17/2002

Sponsored Program
SBIR
Awarding Agency
DOD : MDA
Total Award Amount
$450,000
Award Phase
2
Solicitation Topic Code
BMDO97-007
Principal Investigator
David Hoylman

Company Information

J A Woollam Company

645 M Street Suite 102
Lincoln, NE 68508
   (402) 477-7501
   sales@jawoollam.com
   www.jawoollam.com
Location: Single
Congr. District: 01
County: Lancaster

Phase I

Contract Number: DASG60-97-M-0136
Start Date: 4/1/1997    Completed: 9/30/1997
Phase I year
1997
Phase I Amount
$60,000
Thermal control of a space satellite in orbit is usually accomplished by balancing the energy emitted by the satellite as infrared radiation against the energy dissipated by internal electrical (and other) sources plus energy absorbed from the environment. Due to changing conditions as the satellite orbits there is strong need for a simple thermal control surface operable with low electric power. Components of an electrochromic thin film structure operating in the mid-infrared (1 to 14 microns) have been demonstrated at the University of Nebraska. Preliminary data show a potential for switching of up to 70% of the emissivity in the mid-infrared. The purpose of the Phase I proposal is to test the feasibility of a electrochromically switchable large area thermal control surfaces over the spectral range 1 to 30 microns. This covers most of the Blackbody radiation spectrum of a spacecraft at a few degrees Celsius. The proposed work partners the materials preparation capability at the University of Nebraska with the extensive optical and thermal measurements experience and capability at the J. A. Woollam Co., Inc.. In Phase II we will build and test large area devices and transfer the deposition technology to a commercial optical coatings company. The benefits of this research and development when carried through Phases I, II and III will be operating commercially available spacecraft thermal infrared optical switches. These also have application in laser defense weapons systems and infrared optoelectronics.

Keywords:
Satellite Thermal Control, Electrochromics, Infrared Optical Switching

Phase II

Contract Number: DASG60-98-C-0054
Start Date: 2/2/1998    Completed: 1/1/2000
Phase II year
1998
Phase II Amount
$390,000
Thermal control of a space satellite is usuall yaccomplished by balancing the energy emitted as infrared radiation against the energy dissipated by internal electrical (and other) sources plusenergy absorbed from the enviornment. Due tochanging conditions as the satellite orbits thereis strong need for a simple thermal controlsurface operable with low electric power.Electrochromic optical switches showelectrochromic infrared optical switching devicehas been demonstrated. These devices were madewith thin layers of WO3, organic ion conductor,and NiO ion storage layer. Devices weresuccessfullly operated, covering the spectralrange 300 nm to 30 microns, and reversible switching demonstrated repeatedly. We now seekthe opportunity to carry out Phase II research toachieve large-area, long-life, thermal controlsurfaces, and to be ready for Phase IIIcommercialization.

Keywords:
Optical Switches, Satellited Thermal Control Surfaces, Electrochromics, Infrared