Exquadrum, Inc.

Address

FL
Jupiter, FL, 33477-5096

http://www.exquadrum.com

Information

DUNS: 126112387
# of Employees: 20

Ownership Information

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

Award Charts




Award Listing

  1. Low-Cost Turbopump for Expendable Launch Technology

    Amount: $1,499,969.00

    Extremely low-cost, lightweight, and high performance expendable upper stages are critical to meeting DARPAs goals for low-cost launch. Engines are the most expensive element of the upper stage, and ...

    SBIRPhase II2016Department of Defense Defense Advanced Research Projects Agency
  2. Advanced Research for Controllable, Highly Efficient Rocket Propulsion (ARCHER)

    Amount: $983,986.00

    The objective of the proposed Advanced Research for Controllable, Highly Efficient Rocket Propulsion (ARCHER) Phase II is to develop and demonstrate an innovative, high-performing solid propellant tha ...

    SBIRPhase II2015Department of Defense
  3. Novel Upper Stage Engine Cycle

    Amount: $348,189.00

    ABSTRACT: Exquadrum, Inc. proposes to develop an innovative and advanced, low-cost, high-performance, cryogenic upper stage engine cycle. The SLATE engine is a modified dual-bleed expander cycle tha ...

    SBIRPhase II2015Department of Defense
  4. Multi-Mode On-Board Power Generation

    Amount: $149,998.00

    ABSTRACT: Exquadrum, Inc. proposes to develop an innovative multi-mode power generation system for hypersonic flight vehicles. This system produces the required power output that the flight vehicle de ...

    STTRPhase I2015Department of Defense
  5. Low-Cost Turbopump for Expendable Launch Technology

    Amount: $149,905.95

    Extremely low-cost, lightweight, and high performance expendable upper stages are critical to meeting DARPAs goals for low-cost launch. Engines are the most expensive element of the upper stage, and ...

    SBIRPhase I2015Department of Defense Defense Advanced Research Projects Agency
  6. Low-Cost High-Performance Non-Toxic Self-Pressurizing Storable Liquid Bi-Propellant Pressure-Fed Rocket Engine

    Amount: $124,996.00

    Exquadrum proposes a high-performance liquid bi-propellant rocket engine that uses propellants that are non-toxic, self-pressurizing, and low cost. The proposed engine and propellants provide the sam ...

    SBIRPhase I2014National Aeronautics and Space Administration
  7. Powder Rocket with Improved Mass-fraction and Agility (PRIMA)

    Amount: $1,051,266.00

    The objective of the proposed research and development effort is to demonstrate the feasibility of an innovative approach to high performance and highly controllable solid rocket propulsion for advanc ...

    SBIRPhase II2014Department of Defense Missile Defense Agency
  8. Powder Rocket with Improved Mass-fraction and Agility (PRIMA)

    Amount: $149,986.00

    The objective of the proposed research and development effort is to demonstrate the feasibility of an innovative approach to high performance and highly controllable solid rocket propulsion for advanc ...

    SBIRPhase I2013Missile Defense Agency Department of Defense
  9. Rocket Nozzle Thrust Diverter

    Amount: $738,364.00

    ABSTRACT: Exquadrum proposes to continue development of its rocket nozzle thrust diverter, which was successfully demonstrated in Phase I. The innovative thrust diverter operates separate from the e ...

    SBIRPhase II2013Department of Defense
  10. Hybrid Propulsion for Upper-Stage Boosters

    Amount: $699,991.00

    The objective of the proposed research and development effort is to demonstrate the feasibility of an innovative approach to high-performance hybrid propulsion for upper-stages. The missions for thes ...

    STTRPhase II2013National Aeronautics and Space Administration

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