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Thrust Single Seat

SKU: 53-200C

Spacecraft Valve by Moog (11 more products)
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The 53-200C from Moog is a Spacecraft Valve with Mass 409 g, Supply Voltage 20 to 32 V, Power Consumption 47.6 W, Operating Pressure 19 bar, Burst Pressure 49.3 bar. More details for 53-200C can be seen below.

Product Specifications

Product Details

  • Part Number
    53-200C
  • Manufacturer
    Moog
  • Description
    Thrust Single Seat

General Parameters

  • Mission
    Mars Science Laboratory (MSL), AEHF, TacSat-2, ISS & Resupply (Columbus, MPLM, and ATV), QinetiQ Comsat, BepiColombo
  • Mass
    409 g
  • Valve Type
    Bipropellant Thruster Valve
  • Supply Voltage
    20 to 32 V
  • Power Consumption
    47.6 W
  • Operating Pressure
    19 bar
  • Burst Pressure
    49.3 bar
  • Proof Pressure
    31 bar
  • Response Time
    20 to 30 ms
  • External Leakage Time
    1.0 x 10-4 scc/s
  • Internal Leakage Time
    5 scc/hr
  • Life Cycle
    5000 Cycles
  • Operating Temperature
    4.4 to 93.3 Degree C

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