Multi Layer Insulation (MLI) / Super Insulation（SI)

Multi Layer Insulation (MLI) / Super Insulation（SI)

Shipping:
Ask
Satellite Size:
Price: Ask
Many experience of space development such as H-II Transfer Vehicle “KOUNOTORI”(2009-2018, JAXA) and Japanese Experiment Module “KIBO” in International Space Station (ISS)(2008, JAXA).
  • Feature

    ･ Protects the surface of spacecraft and artificial satellites from the radiant heat of the sun.


    ･ Polyimide grades are excellent in heat resistance.


    ･ Integrated production from raw material polyimide film in KANEKA


  • Specification
    (Single side or both sides) Aluminium Coated Polyimide film
    Thickness (μm)
    12, 25, 50
    Weight (g/m2)
    19, 38, 74
    Solar Absobance (αs) (25μm thickness Single side Aluminum Coated Polyimide film)
    0.07(Aluminum side), 0.34(Polyimide side)
    Normal Emittance (εN) (25μm thickness Single side Aluminum Coated Polyimide film)
    0.04(Aluminum side), 0.68(Polyimide side)
    *These dada are not guaranteed values but the typical measurement values at our company.
  • Miscellaneous

    ･ Price and lead time depend on specification.


    ･ You can search for the specifications in JAXA's "Materials Database System". http://matdb.jaxa.jp/main_e.html


    ･ International Space Station - Japan Aerospace Exploration Agency: JAXA http://iss.jaxa.jp/en/htv/


    ･ Our company MLI website http://www.kaneka.co.jp/en/business/qualityoflife/eit_005.html


Similar Products