Istar Inc.

Basic Information

406 Alta Ave
Santa Monica, CA, 90402

Company Profile

n/a

Additional Details

Field Value
DUNS: n/a
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: n/a


  1. 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 ...

    SBIR Phase II 1988 National Aeronautics and Space Administration
  2. DETONATION DUCT GAS GENERATOR DEVELOPMENT

    Amount: $50,000.00

    N/A

    SBIR Phase I 1987 National Aeronautics and Space Administration
  3. 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 ...

    SBIR Phase I 1986 ArmyDepartment of DefenseDepartment of Defense
  4. 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 ...

    SBIR Phase I 1985 National Aeronautics and Space Administration
  5. 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 ...

    SBIR Phase I 1983 National Aeronautics and Space Administration

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