Award Data

Alameda Applied Sciences Corporation (AASC) proposes to develop and commercialize stable, more durable and less expensive optical multi-layer coatings that can turn a visor into a display screen for helmet mounted display devices, with minimal impact onthe pilot's overall visual acuity. The innovation proposed is to use filtered cathodic arc plasmas to deposit high density optical coatings that a ...

Alameda Applied Sciences Corporation proposes to develop a new type of nano-thruster electric engine for highly parallel, distributed constellations of nano-satellites and other space propulsion applications. A key feature of the proposed Phase-I is theuse of an Inductive Energy Store (IES) driver to power the vacuum arc nano-thruster, which has a mass of 90% PPU efficiency from 1-10 W. The provin ...

Alameda Applied Sciences Corporation (AASC) proposes to develop a new type of high voltage, high power diamond switch potentially capable of switching GW power levels at ~100 kV. The basic element of this switch is a thin disk of natural or CVD diamondthat supports up to 25 kV, is triggered into conduction by UV radiation, achieves rise/fall times

A 24-month Phase II project is proposed to develop and implement models that capture the fidelity of high fidelity physics-based (HFPB) models in a fast-running format. It is anticipated that such models will be incorporated in certain modules of theModular Effectiveness/Vulnerability Assessment (MEVA) code developed for and currently used by the Air Force for assessing munitions effectiveness an ...

A 24-month Phase II project is proposed to develop and implement models that capture the fidelity of high fidelity physics-based (HFPB) models in a fast-running format. It is anticipated that such models will be incorporated in certain modules of theModular Effectiveness/Vulnerability Assessment (MEVA) code developed for and currently used by the Air Force for assessing munitions effectiveness an ...

This proposal describes a novel, high thrust density Detonation Wave Engine (DWE) applicable to the Mach range of 0 to 3. The geometry of this novel engine concept naturally provides for integration into a new Combined Cycle Engine with Ramjets. The concept is an intermittent combustion jet engine that harnesses travelling detonation waves to accomplish compression and chemical reaction. The goal ...

An innovative actively cooled structure concept is proposed which integrates proven cooling techniques and state-of-the-art fabrication methods to extend the maximum combustor wall temperature, thereby reducing cooling requirements and aircraft weight while improving engine performance. Specifically, CONvective and TRANspiration cooling (CONTRAN) are uniquely combined, relying on hydrogen coolant ...

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The objective of this SBIR project is to develop enhanced capabilities to evaluate solid rocket motors (SRMs) using x-ray computed tomography (CT) inspection. In Phase I, approaches were defined for developing technology to improve CT inspectioncapabilities. In Phase II, the technology will be developed and incorporated in practical tools to be delivered to OO-ALC at Hill AFB, where Air Force mi ...

The objective of this SBIR project is to develop enhanced capabilities to evaluate solid rocket motors (SRMs) using x-ray computed tomography (CT) inspection. In Phase I, approaches were defined for developing technology to improve CT inspectioncapabilities. In Phase II, the technology will be developed and incorporated in practical tools to be delivered to OO-ALC at Hill AFB, where Air Force mi ...