Monopropellant Tank with Stiff-Plastic Separation Device (Diaphragm)

    • Monopropellant Tank with Stiff-Plastic Separation Device (Diaphragm)

    Purpose:
    Phobos Sample Return Mission - International Program: Return Spacecraft Propulsion System.
    Year of release: 2011
    Flight qualification of the product:
    Letter "O", flight use
    Possibility to adapt the product to customer requirements: Yes
    Submit application


    Parameter Value
    Propellant UDMH, NTO
    Operating Pressure, not over 1.67 MPa
    Mass 5.2 kg
    Volume of Propellant Compartment 30.8 dm³
    Unused Propellant Residue after Expulsions, not over 0.65 dm³
    Allowable Helium Leak during Leakage Test, l·μm of He /s, not over 1 · 10ˉ³
    Allowable Leak Rate throughout Service Life, l·μm of He /s, not over 2.33 · 10ˉ²
    Inner Compartment Cleanness Russia State Standard GOST 17216, Class 5
    Guaranteed Service Life 15 years

    Description

    Propellant storage and feed to liquid propellant thrusters.

    Legal information
    Please note that this site is for informational purposes only and under no circumstances is not a public offer determined by the provisions of the Part 2 Article 437 of the Civil code of the Russian Federation. Information on this site may be changed or supplemented.