Spacecraft Sub Systems

Hydrazine Reaction Control System

Hydrazine Reaction Control System

Specifications

  • Operating Media

    GN2 Pressurant, Hydrazine Propellant

  • Operating Pressure

    377 – 72.5 psia (26 – 5 bar)

  • Propellant Volume

    ± 882 in3 (± 14.4 L)

  • Nominal Thruster Performance

    1.1 N – 0.25 N

  • Operating Temperature

    50°F - 122°F (10°C - 50°C)

  • Nominal Voltage

    28 Vdc

  • Dry Mass

    < 16.5 lbm (<7.5 kg)

  • Overall Dimensions

    33.3 x 33.3 x 36.3 in (847 x 847 x 923 mm)

  • Construction

    Stainless steel tubing, fittings and components except Titanium tank, all GTAW orbital welded – 40 total welds

All of our products are flexible and customizable to meet your specific needs. Please contact us for more information.

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Contact Us

For Additional Information Regarding any of our Propulsion Control Products:

Bill Vogt

Spacecraft Fluid Controls Sales Manager

+1-716-687-4109