SBIR/STTR Research Award

Low-Erosion and Affordable Nozzles for Advanced Air-to-Air Missiles

Award identifier b5d1099284184f81a0037b81ae94c65eb4c6f7ceefbcb6ac5590bf204b54b4e5Awarding agency Department of Defense · Navy

Award amount

$149,367

Program and phase

SBIR · Phase I

Award year

2012

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Award details

Awarding agency
Department of Defense
Branch
Navy
Recipient company
KNOBLEY TECHNICAL ASSOCIATES, LLC
Proposal award date
2012-06-12
Contract end date
2013-10-08
UEI
FBXSUUJNJF49
Solicitation number
2012.1
Topic code
N121-014

Research abstract

Knobley Technical Associates, LLC's baseline Phase I proposed program for the Navy's SBIR Solicitation Topic Number N121-014 for Low-Erosion and Affordable Nozzles for Advanced Air-to-Air Missiles will identify and evaluate in a trade study, a series of emerging and innovative nozzle technologies and design architectures that can be cost effectively used in high-performance reduced-signature energy managed dual pulse solid propellant rocket motor propulsion systems for next generation advanced tactical air supremacy missiles. As planned, KTA's proposed Phase I SBIR program will seamlessly transition from identifying and selecting a candidate high performance nozzle system design archecture and material implimentation in the 5 task baseline program phase into a three task Option task in which a prototype nozzle system with the most promising design features and technologies emerging from the baseline trade studies will be designed, fabricated and demonstrated in a rocket motor static test firing to demonstrate the operational functionality and feasibility of the affordable, high performance nozzle system to withstand the high temperature, oxidative, long-duration, multi-thermal shock environments as would be induced in a tactical rocket motor operational application. KTA's nozzle material trade studies will include evaluation of state of the art nozzle insulation materials and erosion resistant throat materials as well as the emerging Ceramic Matrix Composite, boundary layer cooling technologies, carbon/silica carbide type materials, pyrolytic graphite and the electroformed high temperature resistant Re and Re/W metal alloy type shell structures and integration approaches for integrating into a tactical rocket motor nozzlesystem.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

9 SBIR/STTR records share this UEI (2007–2024). Reported award amounts total $5,655,358. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense

Agency intelligence

Department of Defense

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