SBIR/STTR Research Award

Porosity Gradient in Hybrid Composite Structure for Thermal Protection

Award identifier 11e79c0a1abc1e6a666671b6002e4c9bc33f0a433947d28a3f16d6c93501f7c1Awarding agency Department of Defense · Air Force

Award amount

$99,998

Program and phase

STTR · Phase I

Award year

2012

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
LUNA INNOVATIONS INCORPORATED
Proposal award date
2011-11-24
Contract end date
Not reported
UEI
SJHFCDGKJJC5
Solicitation number
2010.B
Topic code
AF10-BT27

Research abstract

ABSTRACT: Many military and aerospace platforms, including a number of airborne and spaceborne vehicles, significantly benefit from new materials that save weight and improve performance. Thermal protection systems (TPS) and extremely high temperature structures are required for a range of hypersonic air and space vehicles. For example, over 20,000 thermal protection ceramic tiles are usually installed on the outside of the Space Shuttle. However, most of the currently used tiles that protect the shuttle from extreme temperature have non-load bearing capability due to their highly porous foam structure. As reported, the loss of the US Space Shuttle Columbia in 2003 was caused by the mechanical failure of some tiles on the orbiter. Additionally, the replacement of damaged tiles is difficult and time-consuming. There is a critical need to develop a lightweight TPS technology that increases specific load bearing capability while providing sufficient thermal insulating properties. In this program, Luna Innovations teaming with an academic partner proposes to address this critical need by developing a lightweight, porous, hybrid ceramic composite structure that provides enhanced load bearing and thermal management capabilities. Both computational modeling and experimental study will be addressed to demonstrate the technology feasibility. BENEFIT: If successful, this development effort will yield a lightweight hybrid ceramic composite system that can provide sufficient thermal protection against extremely high temperature (e.g., 2000-3000 degrees F) and enhanced load-bearing capabilities. This novel technology will have significant applications in a range of hypersonic airborne and spaceborne vehicles like the Boeing X-51 Scramjet and the future spacecraft programs as load-bearing thermal protection systems. In addition to the military applications, a variety of civilian applications in aircrafts, automobiles, and structural thermal management systems would also benefit from the developed lightweight hybrid ceramic materials.

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

994 SBIR/STTR records share this UEI (1991–2026). Reported award amounts total $336,438,763. 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, Department of Health and Human Services, National Science Foundation, Environmental Protection Agency

Agency intelligence

Department of Defense

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