THIS PROJECT WILL DEMONSTRATE THE BENEFITS OF A PARTIAL EMISSION PUMP COUPLED WITH A ZERO NET POSITIVE SUCT…
Award details are derived from public USAspending.gov records. Not a bid recommendation.
Award details
- Award ID
- NNX09CB78C
- Contractor
- Awarding agency
- National Aeronautics and Space Administration
- Sub-agency / office
- National Aeronautics and Space Administration
- Award amount
- $0
- Period of performance
- Sep 29, 2009 – Sep 28, 2011
- NAICS
- 541712 — Research and Development in the Physical, Engineering, and Life Sciences
- PSC
- PSC AR11
- Place of performance
- CO
Public award description
THIS PROJECT WILL DEMONSTRATE THE BENEFITS OF A PARTIAL EMISSION PUMP COUPLED WITH A ZERO NET POSITIVE SUCTION PRESSURE INDUCER DESIGN TO ACHIEVE ROBUST, DEEP THROTTLING CAPABILITY. THIS PUMP APPLICATION IS WELL SUITED FOR 5K TO 15K LBF THRUST RANGE ROCKET ENGINES.
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