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Istar Inc.

Company Information
Address
406 Alta Ave
Santa Monica, CA 90402
United States
Information

UEI: N/A

# of Employees: N/A
Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: No

Award Charts




Award Listing

  • Record 1 TO 6

  1. Venus Altitude Cycling Balloon

    Amount: $104,015.00

    The ISTAR Group ( IG) and team mate Thin Red Line Aerospace (TRLA) propose a Venus altitude cycling balloon (Venus ACB), an innovative superpressure balloon architecture that is ideally suited to clou ...

    SBIRPhase I2014National Aeronautics and Space Administration

  2. DETONATION DUCT GAS GENERATOR DEVELOPMENT

    Amount: $500,000.00

    IT IS PROPOSED TO INVESTIGATE EXPERIMENTALLY THE PERFORMANCEOF A DETONATION DUCT GAS GENERATOR WHICH IN THEORETICAL STUDIES OF GAS TURBINE PERFORMANCE WAS SHOWN TO INCREASE THEEFFICIENCY OF A PRESSURE ...

    SBIRPhase II1988National Aeronautics and Space Administration

  3. DETONATION DUCT GAS GENERATOR DEVELOPMENT

    Amount: $50,000.00

    N/A

    SBIRPhase I1987National Aeronautics and Space Administration

  4. IN AN ENERGETIC MATERIAL

    Amount: $37,831.00

    WE PROPOSE A DETAILED STUDY OF THE DYNAMICS OF A DETONATION WAVE IN A MODEL OF A DENSE ENERGETIC MATERIAL BY THE METHOD OF MOLECULAR DYNAMICS. OUR PURPOSE IS TO INVESTIGATE THE ROLE OF "HOT SPOTS" IN ...

    SBIRPhase I1986Department of Defense Army

  5. PROPOSED HERE IS A DEMONSTRATION OF THE EFFECTIVENESS OF REDUCE COMPRESSOR REEQUIREMENTS AND SPECIFIC FUEL CONSUMPTION WHILE SIGNIFICANTLY INCREASING THE THRUST COEFFICIENT.

    Amount: $49,985.00

    PROPOSED HERE IS A DEMONSTRATION OF THE EFFECTIVENESS OF REDUCE COMPRESSOR REEQUIREMENTS AND SPECIFIC FUEL CONSUMPTION WHILE SIGNIFICANTLY INCREASING THE THRUST COEFFICIENT. THE PROPOSED PROGRAM IS BA ...

    SBIRPhase I1985National Aeronautics and Space Administration

  6. THIS PROGRAM IS TO DEMONSTRATE THE VALIDITY OF A RESULT OBTAINED IN SIMPLIFIED THERMODYNAMIC CYCLE ANALYSIS WHICH INDICATED THAT MAJOR GAINS IN EFFICIENCY COULD BE ACHIEVED IF GAS TURBINES RELEASED HEAT IN DETONATION WAVES RATHER THAN IN CONVENTIONAL

    Amount: $49,000.00

    THIS PROGRAM IS TO DEMONSTRATE THE VALIDITY OF A RESULT OBTAINED IN SIMPLIFIED THERMODYNAMIC CYCLE ANALYSIS WHICH INDICATED THAT MAJOR GAINS IN EFFICIENCY COULD BE ACHIEVED IF GAS TURBINES RELEASED HE ...

    SBIRPhase I1983National Aeronautics and Space Administration
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