Prospector®

Polyamide (Nylon) by Envalior

Product Availability Product Description
Stanyl® TW261F5 Africa & Middle East
25% Glass Fiber Reinforced, Heat Stabilized
Stanyl® TW271B3 Africa & Middle East
15% Carbon Fiber Reinforced, Heat Stabilized, Wear and Friction Modified Stanyl® TW271B3 is a friction-modified high heat polyamide that offers excellent creep resistance, strength, stiffness and fatigue resistance, not only at ambient temperatures but especially at high temperatures, while at the same time providing cycle-time advantages and excellent flow. TW271B3 has an excellent track-record in gear applications. Design Challenge Wear & Friction
Stanyl® TW271B6 Africa & Middle East
30% Carbon Fiber Reinforced, Heat Stabilized, Wear and Friction Modified Stanyl® TW271B6 is a friction-modified high heat polyamide that offers excellent creep resistance, strength, stiffness and fatigue resistance especially at high temperatures in combination with cycle-time advantages and excellent flow. TW271B6 has an excellent track-record in gear applications. Design Challenge Wear & Friction
Stanyl® TW271F6 Africa & Middle East
30% Glass Fiber Reinforced, Heat Stabilized, Wear and Friction Modified Stanyl® TW271F6 is a friction-modified high heat polyamide that offers excellent creep resistance, strength, stiffness and fatigue resistance especially at high temperatures in combination with cycle-time advantages and excellent flow. TW271F6 has an excellent track-record in gear applications.
Stanyl® TW271F8 Africa & Middle East
40% Glass Fiber Reinforced, Heat Stabilized, Wear and Friction Modified Design Challenge Wear & Friction
Stanyl® TW272F6 Africa & Middle East
30% Glass Fiber Reinforced, Heat Stabilized, Wear and Friction Modified
Stanyl® TW275F6 Africa & Middle East
30% Glass Fiber Reinforced, Heat Stabilized, Wear and Friction Modified Design Challenge Wear & Friction
Stanyl® TW278F10 Africa & Middle East
50% Glass Fiber Reinforced, Heat Stabilized, Wear and Friction Modified Stanyl® TW278F10 is a friction-modified high heat polyamide that offers excellent creep resistance, strength, stiffness and fatigue resistance especially at high temperatures in combination with cycle-time advantages and excellent flow. TW278F10 has an excellent track-record in gear applications. Design Challenge Wear & Friction
Stanyl® TW300 Africa & Middle East
Heat Stabilized Stanyl® TW300 is a non-reinforced high heat polyamide that offers excellent wear & friction properties in combination with outstanding creep resistance, strength, stiffness and fatigue resistance especially at high temperatures in combination with cycle-time advantages and excellent flow.
Stanyl® TW341 B-MB Africa & Middle East
Heat Stabilized, Lubricated Stanyl® TW341 is a V2 UL-rated, non-reinforced high heat polyamide that offers excellent wear & friction properties in combination with outstanding creep resistance, strength, stiffness and fatigue resistance especially at high temperatures in combination with cycle-time advantages and excellent flow.
Stanyl® TW341 Africa & Middle East
Heat Stabilized, Lubricated Stanyl® TW341 is a V2 UL-rated, non-reinforced high heat polyamide that offers excellent wear & friction properties in combination with outstanding creep resistance, strength, stiffness and fatigue resistance especially at high temperatures in combination with cycle-time advantages and excellent flow. Design Challenge Wear & Friction
Stanyl® TW341-B Africa & Middle East
Heat Stabilized, Lubricated Stanyl® TW341-B is a non-reinforced high heat polyamide that offers excellent wear & friction properties in combination with outstanding creep resistance, strength, stiffness and fatigue resistance especially at high temperatures in combination with cycle-time advantages and excellent flow. Design Challenge Wear & Friction
Stanyl® TW341-FC Africa & Middle East
Heat Stabilized, Lubricated, Food Contact Quality Design Challenge Wear & Friction
Stanyl® TW341H Africa & Middle East
Heat Stabilized, Lubricated
Stanyl® TW341-N Africa & Middle East
Heat Stabilized, Lubricated Stanyl® TW341-N is a non-reinforced high heat polyamide that offers excellent wear & friction properties in combination with outstanding creep resistance, strength, stiffness and fatigue resistance especially at high temperatures in combination with cycle-time advantages and excellent flow. Design Challenge Wear & Friction
Stanyl® TW341-NH Africa & Middle East
Heat Stabilized, Lubricated
Stanyl® TW363 Africa & Middle East
Heat Stabilized, Impact Modified Stanyl® TW363 is an impact-modified high heat polyamide that offers excellent wear & friction properties in combination with outstanding creep resistance, strength, stiffness and fatigue resistance especially at high temperatures in combination with cycle-time advantages and excellent flow.
Stanyl® TW371 Africa & Middle East
Heat Stabilized, Wear and Friction Modified Stanyl® TW371 is a friction-modified high heat polyamide that offers excellent wear & friction properties in combination with outstanding creep resistance, strength, stiffness and fatigue resistance especially at high temperatures in combination with cycle-time advantages and excellent flow. Design Challenge Wear & Friction
Stanyl® TW376 Africa & Middle East
Unreinforced, Heat Stabilized, Wear and Friction Modified
Stanyl® TW441 Africa & Middle East
High Viscosity, Heat Stabilized, Lubricated Stanyl® TW441 is a non-reinforced high heat polyamide that offers excellent wear & friction properties in combination with outstanding creep resistance, strength, stiffness and fatigue resistance especially at high temperatures in combination with cycle-time advantages and excellent flow. Design Challenge Wear & Friction
Tepex® dynalite 101-RG600(x)/47% Africa & Middle East
Tepex® dynalite 101-RG600(x)/47%Roving Glass - PA66 consolidated composite laminate The datasheet is valid for this specific composition only, the characteristics of composites depend on reinforcement level and fiber orientation. Non-standard thickness may alter some or all of these properties. The data listed here are given as average product properties and should not be used to establish specification limits nor used alone as basis of design. The underlying tests were conducted at room temperature and (where possible) with 2 mm specimen thickness. For tensile and flexural tests a specimen width of 25 mm was used and is highly recommended to achieve representative results.
Tepex® dynalite 101-RGUD600(x)/47% Africa & Middle East
Tepex® dynalite 101-RGUD600(x)/47%Roving Glass - PA66 consolidated composite laminate The datasheet is valid for this specific composition only, the characteristics of composites depend on reinforcement level and fiber orientation. Non-standard thickness may alter some or all of these properties. The data listed here are given as average product properties and should not be used to establish specification limits nor used alone as basis of design. The underlying tests were conducted at room temperature and (where possible) with 2 mm specimen thickness. For tensile and flexural tests a specimen width of 25 mm was used and is highly recommended to achieve representative results.
Tepex® dynalite 102-RG600(x)/47% Africa & Middle East
Tepex® dynalite 102-RG600(x)/47%Roving Glass - PA6 consolidated composite laminate The datasheet is valid for this specific composition only, the characteristics of composites depend on reinforcement level and fiber orientation. Non-standard thickness may alter some or all of these properties. The data listed here are given as average product properties and should not be used to establish specification limits nor used alone as basis of design. The underlying tests were conducted at room temperature and (where possible) with 2 mm specimen thickness. For tensile and flexural tests a specimen width of 25 mm was used and is highly recommended to achieve representative results.
Tepex® dynalite 102-RGUD600(x)/47% Africa & Middle East
Tepex® dynalite 102-RGUD600(x)/47%Roving Glass - PA6 consolidated composite laminate The datasheet is valid for this specific composition only, the characteristics of composites depend on reinforcement level and fiber orientation. Non-standard thickness may alter some or all of these properties. The data listed here are given as average product properties and should not be used to establish specification limits nor used alone as basis of design. The underlying tests were conducted at room temperature and (where possible) with 2 mm specimen thickness. For tensile and flexural tests a specimen width of 25 mm was used and is highly recommended to achieve representative results.
Tepex® dynalite 201-C200(x)/45% Africa & Middle East
Tepex® dynalite 201-C200(x)/45%3K Carbon - PA66 consolidated composite laminate The datasheet is valid for this specific composition only, the characteristics of composites depend on reinforcement level and fiber orientation. Non-standard thickness may alter some or all of these properties. The data listed here are given as average product properties and should not be used to establish specification limits nor used alone as basis of design. The underlying tests were conducted at room temperature and (where possible) with 2 mm specimen thickness. For tensile and flexural tests a specimen width of 25 mm was used and is highly recommended to achieve representative results.
Tepex® dynalite 201-C200(x)/50% Africa & Middle East
Tepex® dynalite 201-C200(x)/50%3K Carbon - PA66 consolidated composite laminate The datasheet is valid for this specific composition only, the characteristics of composites depend on reinforcement level and fiber orientation. Non-standard thickness may alter some or all of these properties. The data listed here are given as average product properties and should not be used to establish specification limits nor used alone as basis of design. The underlying tests were conducted at room temperature and (where possible) with 2 mm specimen thickness. For tensile and flexural tests a specimen width of 25 mm was used and is highly recommended to achieve representative results.
Tepex® dynalite 202-C200(x)/45% Africa & Middle East
Tepex® dynalite 202-C200(x)/45%3K Carbon - PA6 consolidated composite laminate The datasheet is valid for this specific composition only, the characteristics of composites depend on reinforcement level and fiber orientation. Non-standard thickness may alter some or all of these properties. The data listed here are given as average product properties and should not be used to establish specification limits nor used alone as basis of design. The underlying tests were conducted at room temperature and (where possible) with 2 mm specimen thickness. For tensile and flexural tests a specimen width of 25 mm was used and is highly recommended to achieve representative results.
Tepex® dynalite 202-C200(x)/50% Africa & Middle East
Tepex® dynalite 202-C200(x)/50%3K Carbon - PA6 consolidated composite laminate The datasheet is valid for this specific composition only, the characteristics of composites depend on reinforcement level and fiber orientation. Non-standard thickness may alter some or all of these properties. The data listed here are given as average product properties and should not be used to establish specification limits nor used alone as basis of design. The underlying tests were conducted at room temperature and (where possible) with 2 mm specimen thickness. For tensile and flexural tests a specimen width of 25 mm was used and is highly recommended to achieve representative results.
Tepex® dynalite 206-C200(x)/45% Africa & Middle East
Tepex® dynalite 206-C200(x)/45%3K Carbon - PA12 consolidated composite laminate The datasheet is valid for this specific composition only, the characteristics of composites depend on reinforcement level and fiber orientation. Non-standard thickness may alter some or all of these properties. The data listed here are given as average product properties and should not be used to establish specification limits nor used alone as basis of design. The underlying tests were conducted at room temperature and (where possible) with 2 mm specimen thickness. For tensile and flexural tests a specimen width of 25 mm was used and is highly recommended to achieve representative results.
Tepex® dynalite 401-C200(2)-FG290(2)/45% Africa & Middle East
Tepex® dynalite 401-C200(2)-FG290(2)/45%Roving Glass - PA66 consolidated composite laminate The datasheet is valid for this specific composition only, the characteristics of composites depend on reinforcement level and fiber orientation. Non-standard thickness may alter some or all of these properties. The data listed here are given as average product properties and should not be used to establish specification limits nor used alone as basis of design. The underlying tests were conducted at room temperature and (where possible) with 2 mm specimen thickness. For tensile and flexural tests a specimen width of 25 mm was used and is highly recommended to achieve representative results.
Tepex® dynalite 401-C200(2)-FG290(4)/45% Africa & Middle East
Tepex® dynalite 401-C200(2)-FG290(4)/45%Roving Glass - PA66 consolidated composite laminate The datasheet is valid for this specific composition only, the characteristics of composites depend on reinforcement level and fiber orientation. Non-standard thickness may alter some or all of these properties. The data listed here are given as average product properties and should not be used to establish specification limits nor used alone as basis of design. The underlying tests were conducted at room temperature and (where possible) with 2 mm specimen thickness. For tensile and flexural tests a specimen width of 25 mm was used and is highly recommended to achieve representative results.
Tepex® dynalite 401-C200(2)-FG290(6)/45% Africa & Middle East
Tepex® dynalite 401-C200(2)-FG290(6)/45%3K Carbon - Filament Glass core - PA66 consolidated composite laminate The datasheet is valid for this specific composition only, the characteristics of composites depend on reinforcement level and fiber orientation. Non-standard thickness may alter some or all of these properties. The data listed here are given as average product properties and should not be used to establish specification limits nor used alone as basis of design. The underlying tests were conducted at room temperature and (where possible) with 2 mm specimen thickness. For tensile and flexural tests a specimen width of 25 mm was used and is highly recommended to achieve representative results.
Tepex® dynalite 402-C200(2)-FG290(2)/45% Africa & Middle East
Tepex® dynalite 402-C200(2)-FG290(2)/45%3K Carbon - Filament Glass core - PA6 consolidated composite laminate The datasheet is valid for this specific composition only, the characteristics of composites depend on reinforcement level and fiber orientation. Non-standard thickness may alter some or all of these properties. The data listed here are given as average product properties and should not be used to establish specification limits nor used alone as basis of design. The underlying tests were conducted at room temperature and (where possible) with 2 mm specimen thickness. For tensile and flexural tests a specimen width of 25 mm was used and is highly recommended to achieve representative results.
Udea™ Akulon® K20HC60 Africa & Middle East
60% Continuous Carbon Fiber Reinforced, Uni-Directional Tape, Heat Stabilized, Black
Udea™ Akulon® K20HG60 Africa & Middle East
60% Continuous Glass Fiber Reinforced, Uni-Directional Tape, Heat Stabilized, Black
Udea™ EcoPaXX® Q20HC60 Africa & Middle East
60% Continuous Carbon Fiber Reinforced, Uni-Directional Tape, Heat Stabilized, Black
Udea™ EcoPaXX® Q20HG60 Africa & Middle East
60% Continuous Glass Fiber Reinforced, Uni-Directional Tape, Heat Stabilized, Black