Wickman Spacecraft & Propulsion Co.

Basic Information

WY
Casper, WY, 82604-1339

Company Profile

n/a

Additional Details

Field Value
DUNS: 26732599
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 3


  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 ...

    SBIR Phase II 2011 National 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 ...

    SBIR Phase I 2010 National 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 ...

    SBIR Phase II 2007 Air 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 ...

    SBIR Phase II 2006 Army 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 ...

    SBIR Phase I 2005 Army 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 ...

    SBIR Phase I 2005 Air Force Department of Defense
  7. IN SITU MARTIAN ROCKET AND "AIR BREATHING" JET ENGINES

    Amount: $397,276.00

    N/A

    SBIR Phase II 1997 National Aeronautics and Space Administration
  8. IN SITU MARTIAN ROCKET AND "AIR BREATHING" JET ENGINES

    Amount: $60,859.00

    N/A

    SBIR Phase I 1996 National Aeronautics and Space Administration
  9. Lox/Kerosene Monopropellant Rocket Engine

    Amount: $59,644.00

    N/A

    SBIR Phase I 1995 National 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 ...

    SBIR Phase I 1992 National Aeronautics and Space Administration

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