SBIR/STTR Research Award

Ceramic Technologies for Shape Stable Hypersonic Monocoque Aeroshells

Award identifier 51e6adb2057736a6ba40c4efc93c0271fdca3654bc5bf416952a444dff338a2cAwarding agency Department of Defense · Air Force

Award amount

$149,922

Program and phase

SBIR · Phase I

Award year

2015

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
PHYSICAL SCIENCES INC.
Proposal award date
2015-06-19
Contract end date
2016-06-19
UEI
RMG1AZ1ZH8Q7
Solicitation number
2015.1
Topic code
AF151-192

Research abstract

ABSTRACT: The PSI Team will develop highly innovative hypersonic vehicle ceramic matrix composite (CMC) structures to significantly advance the state-of-the-art aeroshells that meet the flight requirements of hypersonic vehicles currently under design. The PSI focus is to mature and demonstrate the technologies necessary to manufacture a fully integrated, structurally efficient loadbearing, cost competitive aeroshells. Z-pinning will be used during composite lay-up and cure to locally increase interlaminar strength and create fully integral stiffeners and sub-structure attachment points. Localized regions will have fully integrated, self-healing, compositionally graded, non-silicon containing protective oxide surfaces capable of withstanding higher temperatures than the silicon containing SiC matrices. Novel processing technology will form these tempered regions of the aeroshell that will operate with zero erosion at temperatures well above 3000oF. The PSI production process minimizes the use of process tooling and eliminates the expensive and time consuming machining of dense ceramics. The CMC technology will provide designers the ability to locally change vehicle geometry for higher temperature operation, leading to significant improvements in vehicle performance. This is an important aspect of the PSI approach as cost is a major vehicle design driver and a paramount discriminator amongst the OEMs. BENEFIT: Applications for low cost high temperature aeroshell materials include Department of Defense hypersonic boost-glide vehicles for reconnaissance or weapons systems as well as rocket based combined cycle (RBCC) vehicles for orbital access. Successful development of a low cost manufacturing process for high temperature composite materials and large structures based on silicon carbide will also enable cost effective construction of silicon carbide heat exchangers for aggressive chemical processing and waste treatment. Heat exchanger products offer the largest sustainable market opportunity of $25 million/year.

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

1,763 SBIR/STTR records share this UEI (1983–2026). Reported award amounts total $698,949,224. 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 Health and Human Services, Department of Energy, National Science Foundation, Environmental Protection Agency

Agency intelligence

Department of Defense

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