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Fuel Tank Components

Working Medium Tank MVSK

  • Purpose: Monopropellant propulsion system for spacecraft
  • Flight qualification of the product: Letter "O", flight use
  • Possibility to adapt the product to customer requirements: Yes
ParameterValue
PropellantHydrazine
Operating Pressure, not over1.32 MPa
Mass, not over2.5 kg
Volume of Propellant Compartment8.4±0.1 dm³
Unused Propellant Residue after Expulsions, not over0.2 dm³
Allowable Helium Leak:- Total, l·μm of He/s, not over5.0 · 10ˉ⁴
Allowable Helium Leak:- Diaphragm Leak Test, l·μm of He/s, not over5.0 · 10ˉ³
Inner Compartment CleannessRussia State Standard GOST 17216, Class 5
Guaranteed Service Life12.5 years

Hydrazine storage and feed to liquid propellant thrusters