Aero-plasma, Inc.

Basic Information

23974 Craftsman Rd.
Calabasas, CA, 91302

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: 7


  1. Monopropellant Hydrogen Plasma Ignition System for Hydrogen Rocket Engine

    Amount: $77,038.00

    An innovative Microwave-Powered Monopropellant Hydrogen Plasma Ignition System for hydrogen fueled rocket engines, which develops a plasma using only the hydrogen feed gas to the igniter, is proposed ...

    SBIR Phase I 1996 Air ForceDepartment of DefenseDepartment of Defense
  2. Microwave Powered Plasma On-Orbir Thruster System Using a Non-Resonant Plasma Generator

    Amount: $59,976.00

    An innovative Microwave-Powered Plasma Thruster concept for On-Orbit application is proposed based on its significant ISP magnitude advantages over the electric arcjet thrusters attained by reduction ...

    SBIR Phase I 1994 Air ForceDepartment of DefenseDepartment of Defense
  3. IGNITION AND FLAME FRONT SUSTENANCE OF NAVY AIRCRAFT JET PROPULSION SYSTEMS BY USE OF MICROWAVE IRRADIATION

    Amount: $491,000.00

    AN INNOVATIVE METHOD FOR IGNITION AND FLAME FRONT SUSTENANCE OF JET ENGINE AIRCRAFT PROPULSION SYSTEMS IS PROPOSED. THIS METHOD UTILIZES THE INTERACTION OF CONTROLLED AND CONCENTRATED MICROWAVE ENERGY ...

    SBIR Phase II 1990 NavyDepartment of DefenseDepartment of Defense
  4. NONINTRUSIVE METHOD FOR DETERMINING PLASMA PROFILES IN HYPERSONIC BOUNDARY LAYERS

    Amount: $49,833.00

    COMPRISES IN WIND TUNNEL OPERATIONAL PARAMETERS, RELATIVE TO ACTUAL ATMOSPHERIC FLIGHT, AND INADEQUACINES IN NUMERICAL SIMULATIONS INDICATE THE REQUIREMENT FOR A NONINTRUSIVE DIAGNOSTIC TECHNIQUE WHIC ...

    SBIR Phase I 1990 Air ForceDepartment of DefenseDepartment of Defense
  5. TECHNICAL EVALUATION OF X-RAY SIMULATION PLASMA OPENING SWITCH AND OTHER KEY COMPONENT PERFORMANCE AND SYSTEM INTEGRATIONS

    Amount: $49,869.00

    THE PROPOSED EFFORT IS INTENDED TO PROVIDE IN DEPTH TECHNOLOGICAL SUPPORT TO THE ARNOLD ENGINEERING DEVELOPMENT CENTER (AEDC) FOR THE INTERPRETATION AND EVALUATION OF THE RELATION BETWEEN THE MAJOR PU ...

    SBIR Phase I 1990 Air ForceDepartment of DefenseDepartment of Defense
  6. AN ADVANCED METHOD FOR STAGNATION ENTHALPY ADDITION AND RECONSTRUCTION IN HYPERSONIC WIND TUNNEL TESTING

    Amount: $49,906.00

    THE CHARACTERIZATION OF FLIGHT BEHAVIOR IN THE HIGH-HYERSONIC DOMAIN (MACH 5-20) AND AT ALTITUDES FROM 1-3X10(5) FEET (30-100 KM) HAS GREAT RELEVANCE FOR THE DESIGN AND DEVELOPMENT OF THE AOTV, NASP, ...

    SBIR Phase I 1989 Air ForceDepartment of DefenseDepartment of Defense
  7. IGNITION AND FLAME FRONT SUSTENANCE OF NAVY AIRCRAFT JET PROPULSION SYSTEMS BY USE OF MICROWAVE IRRADIATION

    Amount: $49,403.00

    N/A

    SBIR Phase I 1987 NavyDepartment of DefenseDepartment of Defense

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