Innovative Engineering Solutions Inc
- View government funding actions
- Murrieta, CA 925627060
- Phone: 951-304-7600
- Corporate URL: www.iesnet.com
- Estimated Number of Employees: 20
- Estimated Annual Receipts: $5,000,000
- Business Start Date: 1995
- Contact Person: Michael Gruszczynski
- Contact Phone: 951-304-7600
- Contact Email: mg@iesnet.com
- Business Structure:
- Corporate Entity (Not Tax Exempt)
- Business Type:
- For Profit Organization
- Woman Owned Small Business
- Woman Owned Business
- Subchapter S Corporation
- Industries Served: Other Guided Missile and Space Vehicle Parts and Auxiliary Equipment Manufacturing, Engineering Services, Testing Laboratories
- Product Areas: R&D-MISSILE & SPACE SYS-ENG DEV, R&D- DEFENSE SYSTEM: MISSILE/SPACE SYSTEMS (ENGINEERING DEVELOPMENT), R&D-MISC HARD GOODS-ENG DEV, R&D- DEFENSE SYSTEM: MISCELLANEOUS HARD GOODS (ENGINEERING DEVELOPMENT), OTHER ENERGY (ENGINEERING), R&D- ENERGY: OTHER (ENGINEERING DEVELOPMENT), R&D- SPACE: AERONAUTICS/SPACE TECHNOLOGY (ENGINEERING DEVELOPMENT), R&D-AERO & SPACE TECH-ENG DEV, R&D-OTHER SPACE-ENG DEV, R&D- SPACE: OTHER (ENGINEERING DEVELOPMENT)
Sampling of Federal Government Funding Actions/Set Asides
In order by amount of set aside monies.
- $50,000 - Thursday the 23rd of January 2014
National Aeronautics And Space Administration
NASA SHARED SERVICES CENTER
UNDER A PHASE 1 EFFORT, WE SUCCESSFULLY DEVELOPED AND DEMONSTRATED A SPARK IGNITION CONCEPT WHERE PROPELLANT FLOW DRIVES A VERY SIMPLE FLUID MECHANICAL OSCILLATOR TO EXCITE A PIEZOELECTRIC CRYSTAL. THE PHASE 1 EFFORT EXCEEDED EXPECTATIONS, WITH THE DEVICE DEMONSTRATING RELIABLE IGNITION OF BOTH HYDROGEN AND PROPANE FUELS, AND ACHIEVING IN EXCESS OF 1 MILLION IMPACT CYCLES (40,000 START CYCLES) DURING FATIGUE TESTING WITHOUT MEASUREABLE DEGRADATION. SEVERAL SPIN-OFF CONCEPTS WERE ALSO IDENTIFIED THAT PROVIDE ADDITIONAL OPTIONS FOR IMPROVING SPARK IGNITION SYSTEM DESIGN. DEVELOP SPECIFIC IGNITION SYSTEM DESIGNS FOR TWO CUSTOMER APPLICATIONS, WITH THE INTENTION OF HAVING THESE IGNITION SYSTEMS DEMONSTRATED IN ENGINE GROUND TESTING DURING PHASE 2 AND READY TO START FLIGHT QUALIFICATION IMMEDIATELY FOLLOWING THE PHASE 2 EFFORT. BOTH CUSTOMERS (UNITED LAUNCH ALLIANCE AND PRATT WHITNEY ROCKETDYNE) HAVE EXPRESSED INTEREST AND COMMITMENT IN PARTICIPATING IN THE PHASE 2 ACTIVITY, MAKING ENGINES AND FACILITIES AVAILABLE FOR DEVELOPMENT TESTING, AND INTEGRATING ANY RESULTING VIABLE PRODUCTS INTO THEIR FLIGHT ENGINES. THE ULA APPLICATION IS A NEW GASEOUS BIPROPELLANT H2/O2 ATTITUDE CONTROL THRUSTER, FOR WHICH THE PIEZOELECTRIC IGNITER IS IDEAL AS A SIMPLE, DIRECT IGNITION SOURCE. THE PWR APPLICATION IS FOR AN EVOLVED RL-10 STUDY CURRENTLY UNDERWAY, FOR WHICH THE PIEZOELECTRIC SYSTEM MIGHT BE SCALED UP OR USED AS A PILOT IGNITER FOR A TORCH, OR MAKE USE OF ANOTHER SPIN-OFF CONCEPT THAT WAS IDENTIFIED DURING THE PHASE 1 EFFORT. THE TIMING OF THIS PHASE 2 EFFORT COINCIDES PERFECTLY WITH NEAR TERM NEEDS OF BOTH THESE CUSTOMERS, AS WELL AS FOR OTHER SMALL ENGINE APPLICATIONS IN WORK TO REPLACE CATALYTIC HYDRAZINE ENGINES WITH BI-PROPELLANT ENGINES THAT WILL REQUIRE A SIMPLE AND RELIABLE IGNITION SOURCE. - $45,871 - Thursday the 2nd of May 2013
National Aeronautics And Space Administration
JOHNSON SPACE CENTER
SBIR PHASE III ONE FULL GO2/GCH4 ENGINE ASSEMBLY INCLUDING ELECTRONIC IGNITER - $45,871 - Thursday the 23rd of August 2012
National Aeronautics And Space Administration
JOHNSON SPACE CENTER
SBIR PHASE III ONE FULL GO2/GCH4 ENGINE ASSEMBLY INCLUDING ELECTRONIC IGNITER
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