An Alternative Ice Protection System for Turbine Engine Inlets
Award amount
$599,962Program and phase
SBIR · Phase IIAward year
2006Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- Cox & Company, Inc.
- Proposal award date
- 2005-11-30
- Contract end date
- 2007-11-30
- UEI
- R61JUXLL5FL7
- Solicitation number
- Not reported
- Topic code
- A1.02
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.
- An Alternative Ice Protection System for Turbine Engine Inlets
- Not Available
- Indoor Simulation of Mixed and Snow Icing Conditions
- AN ECONOMICAL HYBRID ANTI-ICING SYSTEM
- AN ECONOMICAL HYBRID ANTI-ICING SYSTEM
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Continuous-Scan Phased Array Measurement Methods for Turbofan Engine Acoustic Testing
- High Channel Count, High Density Microphone Arrays for Wind Tunnel Environments
- High Fidelity Tool for Noise Source Identification
- Plasma Flow Control for Drag Reduction
- Continuous-Scan Phased Array Measurement Methods for Turbofan Engine Acoustic Testing
Research funding history
6 SBIR/STTR records share this UEI (1996–2006). Reported award amounts total $1,409,962. Reported amounts are not federal obligations.
Phases: Phase I, Phase II
Agencies: National Aeronautics and Space Administration