Wickman Spacecraft & Propulsion Co.

Company Information
Address WY
Casper, WY, 82604-1339


Information

DUNS: 26732599

# of Employees: 3


Ownership Information

HUBZone Owned: N

Socially and Economically Disadvantaged: N

Woman Owned: N



Award Charts




Award Listing

  1. Hot Gas TVC For Planetary Ascent Vehicle

    Amount: $594,202.00

    A Mars ascent vehicle (MAV) uses solid rocket motors to propel soil samples into orbit, but the motors cannot provide steering. Flexseal TVC control is planned for the first stage while hydrazine thr ...

    SBIRPhase II2011National Aeronautics and Space Administration
  2. Hot Gas TVC For Planetary Ascent Vehicle

    Amount: $99,971.00

    A Mars ascent vehicle (MAV) uses solid rocket motors to propel soil samples into orbit, but the motors cannot provide steering. Cold gas thrusters are used for initial steering and spin stabilization ...

    SBIRPhase I2010National Aeronautics and Space Administration
  3. Small Launch Vehicles (SLV) Technologies

    Amount: $738,425.00

    Difficulties in using foreign airbases and airspace are constraining the Air Force from striking high-value, time critical targets. A Small Launch Vehicle (SLV) and Common Aero Vehicle (CAV) that de ...

    SBIRPhase II2007Air Force Department of Defense
  4. A Pintle Nozzle With Thrust Vector Control

    Amount: $729,979.00

    Tactical missiles need to control their speed and be able to steer to a wide variety of targets. They usually control their speed with thrust management via pintle nozzles and steer with movable fin ...

    SBIRPhase II2006Army Department of Defense
  5. A Pintle Nozzle With Thrust Vector Control

    Amount: $69,978.00

    Tactical missiles can use pintle nozzles to control speed and wings to steer to targets, but this is inadequate for many targets. To hit a wider variety of targets, tactical missiles must be able to ...

    SBIRPhase I2005Army Department of Defense
  6. Small Launch Vehicles (SLV) Technologies

    Amount: $99,679.00

    Difficulties in using foreign air bases and airspace is constraining the Air Force from striking high-value, time critical targets. The Small Launch Vehicle (SLV) and Common Aero Vehicle (CAV) that ...

    SBIRPhase I2005Air Force Department of Defense
  7. IN SITU MARTIAN ROCKET AND "AIR BREATHING" JET ENGINES

    Amount: $397,276.00

    N/A

    SBIRPhase II1997National Aeronautics and Space Administration
  8. IN SITU MARTIAN ROCKET AND "AIR BREATHING" JET ENGINES

    Amount: $60,859.00

    N/A

    SBIRPhase I1996National Aeronautics and Space Administration
  9. Lox/Kerosene Monopropellant Rocket Engine

    Amount: $59,644.00

    N/A

    SBIRPhase I1995National Aeronautics and Space Administration
  10. HYDROCARBON/LIQUID OXYGEN MONOPROPELLANTS

    Amount: $48,348.00

    LIQUID OXYGEN MONOPROPELLANTS MAY BE PART OF AN EMERGING PROPULSION TECHNOLOGY. THIS PROJECT WILL RESEARCH HOW TO MAKE MONOPROPELLANTS FROM LOW COST, HIGH PERFORMANCE FUEL SOURCES. COAL, KEROSENE AND ...

    SBIRPhase I1992National Aeronautics and Space Administration

Agency Micro-sites

SBA logo
Department of Agriculture logo
Department of Commerce logo
Department of Defense logo
Department of Education logo
Department of Energy logo
Department of Health and Human Services logo
Department of Homeland Security logo
Department of Transportation logo
Environmental Protection Agency logo
National Aeronautics and Space Administration logo
National Science Foundation logo
US Flag An Official Website of the United States Government