Hokenson Co

Address

840 S Tremaine Ave
Los Angeles, CA, 90005

Information

DUNS:
# of Employees: 7

Ownership Information

Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N

Award Charts




Award Listing

  1. LIQUID PROPELLANT GUN SYSTEM DESIGN OPTIMIZATION

    Amount: $368,429.00

    A NUMERICAL SIMULATION OF TRANSIENT TWO-PHASE REACTING FLOW IN LIQUID PROPELLANT GUN SYSTEM IS PROPOSED. SIMULTANEOUS SOLUTION OF THE PROJECTILE POSITION AND INTERNAL FLUID DYNAMICS WILL ALLOW THE OPT ...

    SBIRPhase II1987Army Department of Defense
  2. MINIMUM DRAG BODY DESIGN UTILIZING STATE-OF-THE-ART TURBULENCE MODELS AND (OPTIONAL) LAMINAR FLOW CONTROL FOREBODIES

    Amount: $220,000.00

    UTILIZING AN EXISTING NUMERICAL MODEL OF COUPLED VISCOUS-INVISCID FLOW AROUND AXISYMMETRIC BODIES, THE DESIGN OF MINIMUM DRAG BODIES FOR ARBITRARY MACH AND REYNOLDS NUMBERS SHALL BE SOUGHT. STATE-OFTH ...

    SBIRPhase II1987Air Force Department of Defense
  3. DRAG REDUCTION ON 20 MM AIRCRAFT CANNON PROJECTILES UTILIZING OPTIMAL FOREBODY SHAPING

    Amount: $48,263.00

    UTILIZING AN ITERATIVE-DIRECT DESIGN PROCEDURE TO OBTAIN MINIMUM DRAG AXISYMMETRIC BODIES, DEVELOPED BY THE PRINCIPAL INVESTIGATOR FOR EGLIN AFB, THE PROPOSED RESEARCH SEEKS TO CHARACTERIZE OPTIMAL FO ...

    SBIRPhase I1987Air Force Department of Defense
  4. VARIABLE-ENERGY EJECT FOR MISSILE LAUNCH OVER A WIDE RANGE OF DEPTHS

    Amount: $48,263.00

    UTILIZING EXISTING NUMERICAL SIMULATION TOOLS DEVELOPED BY THE PRINCIPAL INVESTIGATOR AND THE HOKENSON COMPANY, TWO ACTIVE CONTROL CONCEPTS APPLIED TO THE SUBMARINE MISSILE LAUNCH ASSIST GAS GENERATOR ...

    SBIRPhase I1987Navy Department of Defense
  5. EVALUATION OF AN ADD-ON MUZZLE EXHAUST FLOW MANIPULATOR FOR NOISE SUPPRESSION ON LARGE CALIBER GUNS

    Amount: $48,263.00

    UTILIZING NUMERICAL SIMULALTION TOOLS DEVELOPED BY THE PRINCIPAL INVESTIGATOR AND THE HOKENSON COMPANY FOR ARDEC, THE EVALUATION OF A SIMPLE AND LIGHTWEIGHT ADD-ON DEVICE TO MANIPULATE THE MUZZLE EXHA ...

    SBIRPhase I1987Army Department of Defense
  6. A SLOW-BURNING SOLID PROPELLANT WAFER ADD-ON

    Amount: $46,688.00

    UTILIZING AN EXISTING NUMERICAL MODEL OF SWIRLING AND RECIRCULATING BASE FLOW, SIMULATIONS OF PROJECTILE BASE DRAG REDUCTION DUE TO BASE BLEED FLOW SHALL BE CARRIED OUT. MODIFICATIONS TO THE EXISTING ...

    SBIRPhase I1986Air Force Department of Defense
  7. SIGNATURES

    Amount: $46,688.00

    THE PHASE I RESEARCH INVOLVES COMPUTATIONAL WORK, ANALYSIS AND PLANNING FOR PHASE II WORK. THE COMPUTATIONS ARE DIRECT NUMERICAL SIMULATIONS (DNS) OF THE EQUATIONS OF MOTION AT A LOW REYNOLDS NUMBER. ...

    SBIRPhase I1986Army Department of Defense
  8. COMPUTATION LOSS MODELING AND SUPPRESSION

    Amount: $46,688.00

    A COMPREHENSIVE COMPUTATIONAL STUDY OF MULTI-DIMENSIONAL (GAS/CURRENT) FLOW EFFECTS IN INHERENTLY TRANSIENT MHD SYSTEMS IS PROPOSED. TWO CLASSES OF FLOWFIELD NON-UNIFORMITY SHALL BE ADDRESSED: 1) ONE ...

    SBIRPhase I1986Navy Department of Defense
  9. MINIMUM DRAG BODY DESIGN UTILIZING STATE-OF-THE-ART TURBULENCE MODELS AND (OPTIONAL) LAMINAR FLOW CONTROL FOREBODIES

    Amount: $46,688.00

    N/A

    SBIRPhase I1986Air Force Department of Defense
  10. A TWO-DECK BOUNDARY LAYER MODEL OF THE FLOW OVER AN ABLATING (AND/OR TRANSPIRING) SURFACE IS PROPOSED IN ORDER TO COMPUTE THE SURFACE ROUGHNESS AND TEMPERATURE DISTRIBUTION IN THE WALL AND FLOW FOR A GIVEN SET OF WALL AND FREESTREAM CONDITIONS.

    Amount: $36,194.00

    A TWO-DECK BOUNDARY LAYER MODEL OF THE FLOW OVER AN ABLATING (AND/OR TRANSPIRING) SURFACE IS PROPOSED IN ORDER TO COMPUTE THE SURFACE ROUGHNESS AND TEMPERATURE DISTRIBUTION IN THE WALL AND FLOW FOR A ...

    SBIRPhase I1985Air Force Department of Defense

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