WE PROPOSE A HIGH-PRESSURE, REGENERATIVELY-COOLED COMBUSTION CHAMBER THAT USES NOVEL MATERIAL SELECTION FOR…
Award details are derived from public USAspending.gov records. Not a bid recommendation.
Award details
- Award ID
- NNX09CE14P
- Contractor
- Awarding agency
- National Aeronautics and Space Administration
- Sub-agency / office
- National Aeronautics and Space Administration
- Award amount
- $0
- Period of performance
- Jan 22, 2009 – Jul 22, 2009
- NAICS
- 541712 — Research and Development in the Physical, Engineering, and Life Sciences
- PSC
- PSC AR11
- Place of performance
- AL
Public award description
WE PROPOSE A HIGH-PRESSURE, REGENERATIVELY-COOLED COMBUSTION CHAMBER THAT USES NOVEL MATERIAL SELECTION FOR EXTREME REDUCTIONS IN MASS. THESE MATERIALS ARE MANUFACTURED USING PROVEN PROCESSES, PROCESSES IN WHICH OUR TWO TEAM MEMBERS ARE EXPERT. THE COMBUSTION CHAMBER LINER WILL BE MADE OF A HIGH-TEMPERATURE-CAPABLE, LOW DENSITY MATERIAL; THE STRUCTURAL JACKET WILL BE MADE OF A METAL MATRIX COMPOSITE MATERIAL, WITH A TAILORED CTE CLOSE TO THAT OF THE LINER.
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