Concepts Eti Inc as Concepts Nrec
- View government funding actions
- White River Junction, VT 050019486
- Estimated Number of Employees: 120
- Estimated Annual Receipts: $18,000,000
Sampling of Federal Government Funding Actions/Set Asides
In order by amount of set aside monies.
- $87,164 - Friday the 4th of May 2012
Department Of Navy
NAVSUP WEAPON SYSTEMS SUPPORT
TORQUEMETER V250,AI - $72,975 - Friday the 29th of June 2012
Department Of Navy
NAVSUP WEAPON SYSTEMS SUPPORT
TORQUEMETER V35,AIR - $711,620 - Wednesday the 23rd of May 2012
Defense Logistics Agency
DLA AVIATION AT HUNTSVILLE, AL
N/A - $66,017 - Friday the 25th of May 2012
National Aeronautics And Space Administration
MARSHALL SPACE FLIGHT CENTER
PROCUREMENT FOR THE CONCEPTS NREC AGILE PRODUCTS SUPPORT AND LICENSE RENEWAL, IN SUPPORT OF ER31. - $58,109 - Tuesday the 24th of April 2012
Department Of Navy
NAVSUP WEAPON SYSTEMS SUPPORT
TORQUEMETER V250,AI - $35,305 - Wednesday the 29th of August 2012
Department Of Navy
NAVAIR WARFARE CTR AIRCRAFT DIV LKE
TMS ENGINEERING INVESTIGATION - $30,869 - Thursday the 5th of April 2012
Department Of Navy
NAVSUP WEAPON SYSTEMS SUPPORT
DYNAMOMETER,RUN-IN NAVY REPAIR - $30,869 - Thursday the 5th of April 2012
Department Of Navy
NAVSUP WEAPON SYSTEMS SUPPORT
DYNAMOMETER,RUN-IN NAVY REPAIR - $150,000 - Friday the 16th of January 2015
National Aeronautics And Space Administration
NASA SHARED SERVICES CENTER
THE PROPOSED INNOVATION PROVIDES A WAY TO DESIGN LOW FLOW COEFFICIENT INDUCERS THAT HAVE HIGHER CAVITATION BREAKDOWN MARGIN, LARGER BLADE ANGLES, THICKER MORE STRUCTURALLY ROBUST BLADES, AND BETTER OFF-DESIGN FLOW STABILITY THAN THE CURRENT STATE-OF-THE-ART DESIGNS. THE TECHNOLOGY WILL INCREASE THE STRUCTURAL, STABILITY, AND SUCTION MARGIN OF INDUCERS DESIGNED IN THE CURRENTLY ACCEPTABLE FLOW COEFFICIENT RANGE OF ABOUT 0.06 TO 0.1. IN ADDITION, IT WILL ALLOW FOR STABLE AND STRUCTURALLY ROBUST DESIGNS AT MUCH LOWER FLOW COEFFICIENTS THAN PREVIOUSLY THOUGHT POSSIBLE (DOWN TO AT LEAST 0.02) FOR THE CAPABILITY TO OPERATE IN NEAR ZERO NET POSITIVE SUCTION PRESSURE INLET ENVIRONMENTS. THE INNOVATION IS BASED UPON A SYNERGISTIC COUPLING OF CONCEPTS NREC'S PATENTED CAVITATION CONTROL DEVICE WITH A NEW BLADE DESIGN APPROACH THAT TAKES FULL ADVANTAGE OF THE CCD'S CHARACTERISTICS FOR OPTIMAL SUCTION PERFORMANCE. THE TECHNOLOGY SIGNIFICANTLY ENHANCES THE CAPABILITY OF ROCKET ENGINE SYSTEMS THROUGH INCREASED THRUST-TO-WEIGHT, SPECIFIC IMPULSE, SIMPLICITY, OPERATIONAL SAFETY, AND TURBOPUMP LIFE. IT WILL ALSO REDUCE TURBOPUMP AND PROPELLANT TANK WEIGHT AND SYSTEM COSTS BY ELIMINATING BOOST PUMP SYSTEMS AND ALLOWING FOR LIGHTER LOWER PRESSURE TANKS. - $149,995 - Tuesday the 10th of July 2012
Department Of Air Force
FA9300 AFTC PZR
SBIR PHASE 1
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