Manufacturing and Strength Improvement for Thick Carbon-Carbon Laminates
Award amount
$1,496,299Program and phase
SBIR · Phase II – Direct to Phase IIAward year
2014Award details
- Awarding agency
- Department of Defense
- Branch
- Defense Advanced Research Projects Agency
- Recipient company
- Carbon Carbon Advanced Technologies, Inc.
- Proposal award date
- 2014-04-08
- Contract end date
- 2017-05-26
- UEI
- N3NULR7A1A88
- Solicitation number
- 2012.3
- Topic code
- SB133-005
Research abstract
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.
- Extreme Temperature Structures
- Design and Manufacture of a Prototype Hypersonic Glide Vehicle Target Using C-CAT ACC Materials
- Accelerated Processing with Geometry-Specific Pyrolysis Heating Profiles for Production of C-C Hot Structures
- ACC Enhanced with Ceramic Matrix via Reactive Melt Infiltration for Scramjet Duct Applications
- Extreme Temperature Stitched Structures
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Manufacturing and Strength Improvement for Thick Carbon-Carbon Laminates
- Processing of High-Strength Thick C-C Composite Structures using a One-Step Process
- Affordable and Reliable C-C Composites for Thick Load-Bearing Hot Structure
Research funding history
9 SBIR/STTR records share this UEI (2010–2025). Reported award amounts total $7,883,571. Reported amounts are not federal obligations.
Phases: Phase II – Direct to Phase II, Phase II, Phase I
Agencies: Department of Defense, National Aeronautics and Space Administration