Propulsion Science and Technology, Inc.

Basic Information

848 Town Center Drive
Langhorne, PA, -

http://www.propulsionscience.com

Company Profile

n/a

Additional Details

Field Value
DUNS: 165115390
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 6


  1. Methodologies for Accurate Scene Generation of Complex Target Plume Characteristics

    Amount: $99,996.00

    Missile exhaust plume radiant emission is a key observable for any missile defense system using optical sensors. Scene generation has become an important component within MDA to assess the performanc ...

    SBIR Phase I 2012 Department of DefenseMissile Defense AgencyDepartment of Defense
  2. Characterization and Incorporation of Vernier Engines within the Plume Modeling Process

    Amount: $99,986.00

    Vernier engines operating at the same time as the main missile engine can change the overall structure of the engine exhaust plume. This SBIR focuses on the modeling of this interaction using techniq ...

    SBIR Phase I 2012 Department of DefenseMissile Defense AgencyDepartment of Defense
  3. Plume Simulation Using Advanced Image Processing Techniques

    Amount: $435,000.00

    ABSTRACT: An exhaust plume is a primary observable to warning sensors designed to protect low flying aircraft from MANPADS and other hostile threats such as RPG's and small arms fire with tracer ...

    SBIR Phase II 2012 Department of DefenseAir ForceDepartment of Defense
  4. Advanced Reentry Vehicle and Wake Models

    Amount: $999,999.00

    Missile defense systems like AEGIS and THAAD depend upon having prior knowledge of the signature characteristics of the threat missile in order to perform the necessary system functions to defeat the ...

    SBIR Phase II 2012 Department of DefenseMissile Defense AgencyDepartment of Defense
  5. Advanced Reentry Vehicle and Wake Models

    Amount: $99,996.00

    Missile defense systems like THAAD, GBI and AEGIS depend upon having prior knowledge of the signature characteristics of the threat missile in order to perform the necessary system functions to defeat ...

    SBIR Phase I 2011 Department of DefenseMissile Defense AgencyDepartment of Defense
  6. Plume EO-RCS Data Fusion

    Amount: $999,989.00

    The use of models to predict exhaust plume observables such as electro-optical (EO) signatures or radar cross section (RCS) is an integral part of many missile defense activities due to the limited qu ...

    SBIR Phase II 2011 Department of DefenseMissile Defense AgencyDepartment of Defense
  7. Effects of Hardbody-Plume Interactions on Radar Returns

    Amount: $999,984.00

    An effective missile defense requires an understanding of the combined radar signature of a hardbody and plume and a capability for predicting that signature. The proposed program will develop a stat ...

    SBIR Phase II 2011 Department of DefenseMissile Defense AgencyDepartment of Defense
  8. Plume EO-RCS Data Fusion

    Amount: $99,999.00

    The use of models to predict exhaust plume observables such as electro-optical (EO) signatures or radar cross section (RCS) is an integral part of many missile defense activities due to the limited qu ...

    SBIR Phase I 2010 Missile Defense AgencyDepartment of DefenseDepartment of Defense
  9. Effects of Hardbody-Plume Interactions on Radar Returns

    Amount: $99,964.00

    An effective missile defense will require an understanding of the combined radar signature of a hardbody and plume and a capability for predicting that signature. While there is a well developed tech ...

    SBIR Phase I 2010 Missile Defense AgencyDepartment of DefenseDepartment of Defense
  10. High Fidelity Missile Hardbody Plume Interaction Modeling

    Amount: $972,184.00

    The development of innovative sensor technologies requires a complete (both spectral and spatial) knowledge of missile hardbody and exhaust plume signature characteristics of current and evolving thre ...

    SBIR Phase II 2009 Missile Defense AgencyDepartment of DefenseDepartment of Defense

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