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Science and Technology Applications, LLC

Company Information
Address
530 New Los Angeles Avenue, Suite115 # 122
Moorpark, CA 93021-
United States


http://www.sci-tech-apps.com

Information

DUNS: 172773272

# of Employees: 5


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: Yes



Award Charts




Award Listing

  1. Low Toxicity, Non-cryogenic Liquid Propellant Upper Stage Engine

    Amount: $99,986.00

    Our vision for the next generation missile and space propulsion engine is a flexible and non-toxic propulsion technology using HAN/kerosene, offering variable thrust with a high degree of mission tail ...

    STTRPhase I2019Department of Defense Missile Defense Agency
  2. “Green” Liquid Propellant Upper Stage Engine for Air Launched Targets

    Amount: $1,999,990.00

    Our vision for the next generation missile and space propulsion is a flexible and non-toxic propulsion technology using AF-M315E monopropellant, offering variable thrust with a high degree of mission ...

    SBIRPhase II2019Department of Defense Missile Defense Agency
  3. Green Liquid Propellant Upper Stage Engine for Air Launched Targets

    Amount: $149,897.00

    Our vision for a "green" upper stage propulsion is a non-toxic multi-use system using HAN and kerosene, offering variable thrust with a high degree of mission tailoring. Additionally, such system will ...

    SBIRPhase I2018Department of Defense Missile Defense Agency
  4. Lowest Lifecycle Cost (LLC) Propulsion System

    Amount: $1,499,983.00

    ABSTRACT:Future military and commercial spacelift systems will utilize reusable systems, consisting of liquid oxygen/hydrocarbon staged combustion engines, in order to increase the military utility by ...

    SBIRPhase II2015Department of Defense Air Force
  5. Lowest Lifecycle Cost (LLC) Expendable Launch Vehicles

    Amount: $149,915.00

    ABSTRACT: To meet the goals of future generation of ELVs, significant improvements must be made in cost. Current expendable launch vehicles are designed using an optimum performance methodology. Rece ...

    SBIRPhase I2014Department of Defense Air Force
  6. High Performance Cooling Methods for Liquid Rocket Engines

    Amount: $739,572.00

    ABSTRACT: To meet the goals for future generation Air Force LOX/Hydrocarbon booster engines, improvements must be made in performance, operability, reusability, reliability, and cost. To date, operat ...

    SBIRPhase II2013Department of Defense Air Force
  7. High Performance Cooling Methods for Liquid Rocket Engines

    Amount: $149,974.00

    ABSTRACT: To meet the goals for future generation Air Force LOX/Hydrocarbon booster engines, improvements must be made in performance, operability, reusability, reliability, and cost. To date, operat ...

    SBIRPhase I2012Department of Defense Air Force
  8. Novel energetic materials from new polyazide ingredients

    Amount: $99,979.00

    Polynitrogen and high-nitrogen compounds hold great potential for High Energy Density Materials (HEDM). Particular advantages of these compounds are their high energy content, environmentally more ben ...

    STTRPhase I2009Department of Defense Air Force
  9. Variable Thrust and Non-Toxic Liquid Propulsion for Mission Flexibility

    Amount: $99,995.00

    Our vision for the next generation missile propulsion is a flexible and non-toxic system using HAN and a storable fuel candidate, offering variable thrust with a high degree of mission tailoring. Addi ...

    SBIRPhase I2008Department of Defense Air Force
  10. Innovative Deep Throttling, High Performance Injector Concept

    Amount: $99,904.00

    Science and Technology Applications, LLC's (STA) vision for a versatile space propulsion system is a highly throttleable, high performance, and cost effective Liquid Oxygen/Hydrogen engine utilizing i ...

    STTRPhase I2007National Aeronautics and Space Administration
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