TECASINT 2391 black

Polyimide with 15 % MoS2

add to list
product inquiry
request sample
TECASINT 2391 has been developed with 15 % MoS2 from the base polymer TECASINT 2011. It has optimum friction and wear properties in a vacuum, which means it can be used in space travel applications, in a vacuum or in inert gases (techn. dry). The plastic displays low outgassing in accordance with ESA regulation ECSS-Q-70-02.

Facts

Chemical designation
PI (Polyimide)
Color
black
Density
1.53 g/cm3

Main Features

  • high thermal and mechanical capacity
  • very good slide and wear properties
  • low outgassing
  • very good thermal stability
  • good chemical resistance
  • high creep resistance
  • resistance against high energy radiation
  • sensitive to hydrolysis in higher thermal range

Target industries

aircraft and aerospace technology
cryogenic engineering
precision engineering
vacuum technology

Downloads

Datasheet (PDF)

Technical details

  • product-technical-detail-collapse-item-0-lvl-1
    Mechanical properties Value Unit Condition Test Method
    Compressive strain at break 35.6 % 10 mm/min EN ISO 604
    Compression modulus 2000 MPa 1 mm/min EN ISO 604
    Modulus of elasticity
    (flexural test)    		 3900 MPa 2 mm/min DIN EN ISO 178
    Flexural strength 140 MPa 10 mm/min DIN EN ISO 178
    Modulus of elasticity
    (tensile test)    		 4100 MPa 1 mm/min DIN EN ISO 527-1
    Tensile strength 95 MPa 50 mm/min DIN EN ISO 527-1
    Shore hardness 88 Shore D DIN EN ISO 868
    Impact strength (Charpy) kJ/m2 max 7.5 J DIN EN ISO 179-1eU
    Notched impact strength (Charpy) kJ/m2 max 7.5 J DIN EN ISO 179-1eA
    Ball indentation hardness 265 MPa ISO 2039-1
    Compression strength 230 MPa 10 mm/min EN ISO 604
    Elongation at break (tensile test) 3.5 % 50 mm/min DIN EN ISO 527-1
    Compression strength 165 MPa 10mm/min, 10% strain EN ISO 604
    Elongation at break (flexural test) 4.0 % 10 mm/min DIN EN ISO 178
  • product-technical-detail-collapse-item-1-lvl-1
    Thermal properties Value Unit Condition Test Method
    Thermal conductivity W/(k*m) 40°C ISO 8302
    Glass transition temperature 357 C -
    Thermal expansion (CLTE) 4 10-5*1/K 23-100°C, long. DIN EN ISO 11359-1;2
    Thermal expansion (CLTE) 4 10-5*1/K 100-150°C, long. DIN EN ISO 11359-1;2
    Service temperature 260 C long-term -
    Thermal expansion (CLTE) 5.0 - 5.7 10-5*1/K 200-300°C DIN 53 752
    Thermal expansion (CLTE) 4.0 - 4.7 10-5*1/K 50-200°C DIN 53 752
  • product-technical-detail-collapse-item-2-lvl-1
    Other properties Value Unit Condition Test Method
    Flammability (UL94) V0 - corresponding to DIN IEC 60695-11-10;
    HZ-Catalogue yes lbs/in^2 -
    HZ Technical guidelines yes lbs/in^2 -
    Water absorption 0.12 - 0.24 % 24h / 96h (23°C) DIN EN ISO 62
    HZ Aerospace Brochure yes - -
    Outgassing in high vacuum passed ECSS-Q-70-02
    Water absorption 0.53 % 24 h in water, 23°C DIN EN ISO 62
    Water absorption 1.58 % 24 h in water, 80°C DIN EN ISO 62

Stock program