Aero-plasma, Inc.

Address

23974 Craftsman Rd.
Calabasas, CA, 91302

Information

DUNS:
# of Employees: 7

Ownership Information

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

Award Charts




Award Listing

  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 ...

    SBIRPhase I1996Air Force Department 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 ...

    SBIRPhase I1994Air Force Department 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 ...

    SBIRPhase II1990Navy Department 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 ...

    SBIRPhase I1990Air Force Department 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 ...

    SBIRPhase I1990Air Force Department 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, ...

    SBIRPhase I1989Air Force Department 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

    SBIRPhase I1987Navy Department of Defense

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