SBIR/STTR Research Award

Ultra-Lightweight Silicon Carbide Telescope and Advanced Pointer for Combined Multi-Spectral Imager and Active LADAR

Award identifier 72307a86db721b4f0801f597c327b84a035c4a838771e3655063b7115883e14bAwarding agency Department of Defense · Air Force

Award amount

$1,937,434

Program and phase

SBIR · Phase II

Award year

1996

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
SSG, Inc.
Proposal award date
Not reported
Contract end date
Not reported
UEI
Not reported
Solicitation number
Not reported
Topic code
Not reported

Research abstract

Next-generation aircraft and space-based sensors will significantly benefit from a combined aperture multi-spectral passive (visible to LWIR) and active LADAR capability for enhanced target acquisition, ranging, tracking, and discrimination performance; and lower size, weight, power, and cost. Typical DoD missions include advanced AWACS sensors; TMD and NMD interceptors and surveillance systems; cruise missile guidance/control; terrain mapping and photo-reconnaissance; laser guided missiles/weaponry; aircraft landing systems; laser secure links and environmental sensors. The driving technology areas are ultra-lightweight all-reflective telescopes and wide field of regard (FOR), high precision pointing/stabilization control. SSG's proposed concept includes (1) a very lightweight, all-reflective, off-axis, common shared aperture silicon carbide (SiC) telescope for combined, inherently aligned and a thermalized passive/active operation; and (2) a wide FOR, very precise and compact pointer with internal stabilization control. The proposed hardware must satisfy visible level performance under stressing thermal and vibration environments. SSG is proposing a highly innovative SiC process technology that provides very fracture tough (drop on cement floor) and extremely highly damped (50 times better than a metal) structural assembly at very low cost, which is critical for stressing aircraft and rocket applications. The wide FOR pointer uses a meridional 2-axis mirror assembly (size is independent of the large azimuthal angular extent), and a highly innovative fringe counting optical encoder capable of less then 0.5 microrad accuracy, repeatability, and jitter control over the large angular extent. Phase I will develop a combined aperture passive/active sensor concept with supporting analyses and critical technology assessment; Phase II will be a hardware demonstration of critical technology area(s) in a "flight-worthy" configuration.

Technology keywords

Not reported

Agency intelligence

Department of Defense

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