SBIR/STTR Research Award

Advanced Foam Core Composite Insulation for Extended Range Hypersonic Vehicles, Phase II

Award identifier e82f2b432dc7dc82d8e6821105db3a06b7a97f6e6f236aebefae1a9bceea96aeAwarding agency Department of Defense · Air Force

Award amount

$750,000

Program and phase

SBIR · Phase II

Award year

2008

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
ULTRAMET
Proposal award date
2008-03-20
Contract end date
2010-07-20
UEI
N8ZRMWX85NZ6
Solicitation number
2007.1
Topic code
AF071-128

Research abstract

In the Prompt Global Strike (PGS)-Conventional Strike Missile (CSM) program, the Air Force is seeking a mid-term, land-based conventional weapon system capable of striking targets halfway around the globe within an hour of an order to launch. While candidate long-term systems are likely to include conventional variants of current ballistic missile capabilities, the PGS-CSM concept is expected to create new opportunities for hypersonic vehicle technologies, which would offer greater maneuverability approaching a target than would more simple ballistic missile reentry vehicles. Practical application of hypersonic missiles, however, requires development of structures and insulators capable of operating in the very demanding high temperature chemical, thermal, and mechanical environment. In this Phase II project, Ultramet will expand upon the Phase I success in high temperature structural foam-based insulator and refractory composite structure development to design, fabricate, and test aerostructures for application to the PGS-CSM program. Specifically, Ultramet will team with ATK, which will provide system and individual component requirements, Materials Research & Design, which will perform design and analysis, Ocellus, which will optimize aerogel processing and infiltration of Ultramet structural foam insulators, and Carbon-Carbon Advanced Technologies, which will fabricate C/C components for use in combination with Ultramet’s ultrahigh temperature ceramic matrix composite outer shell. Performance will be evaluated through radiant heat testing, and high temperature oxidation behavior will be established through testing at the Air Force LHMEL facility.

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

380 SBIR/STTR records share this UEI (1983–2025). Reported award amounts total $105,154,309. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Energy, National Science Foundation, Department of Transportation, Department of Health and Human Services

Agency intelligence

Department of Defense

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