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Cryogenic-Vacuum Compatible Infrared Scene Projection System (CVC IRSP) Based on the Digital Micromirror Device

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: FA9101-14-C-0029
Agency Tracking Number: F083-255-1999a
Amount: $1,203,043.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: AF083-255
Solicitation Number: 2008.3
Timeline
Solicitation Year: 2008
Award Year: 2015
Award Start Date (Proposal Award Date): 2014-10-27
Award End Date (Contract End Date): 2016-09-20
Small Business Information
P.O. Box 8291
Huntsville, AL 35808-8291
United States
DUNS: 840016109
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 David Beasley
 President/Senior Engineer
 (256) 922-1500
 brett@opticalsciences.com
Business Contact
 David Beasley
Title: President/Senior Engineer
Phone: (256) 922-1500
Email: brett@opticalsciences.com
Research Institution
 Stub
Abstract

ABSTRACT: This document presents Optical Sciences Corporation's SBIR technology transition proposal to complete development of an advanced Cryogenic-Vacuum Compatible Infrared Scene Projector (CVC IRSP) for Wide Field-of-View (WFOV) space sensor testing and to integrate the CVC IRSP into a government owned space simulation chamber. The CVC IRSP will be capable of projecting complex scenes which cover a wide FOV and have a wide temperature range, high spatial resolution, high temperature resolution, and correlated multi-band spectral output. This advanced IRSP technology will be used to support hardware-in-the-loop testing of space-based sensor systems which include Earth observing, strategic, and interceptor sensor systems. BENEFIT: The expected benefits associated with this technology will be two-fold. First, an improved capability for dynamic IR scene projection in a cryo-vacuum environment will be developed. The improved performance parameters will include higher spatial resolution, higher apparent temperatures, improved spatial uniformity, substantially higher frame rates, correlated multi-band unresolved point sources, and a reduced volume. Second, this technology will provide significant cost savings compared to the current CVC IRSP technologies. This advanced IRSP technology will be used to support hardware-in-the-loop testing of space-based sensor systems which include Earth observing, strategic, and interceptor sensor systems.

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

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