| MATERIAL DESCRIPTION: |
Thin wall, flame retarded radiation cross-linked modified polyolefin
heat-shrinkable tubing, assembled as organised cut sleeves in a "ladder" configuration. 3:1 shrink ratio. |
| USE: |
Identification of wires and cables by computer-based printing onto markers.
Sleeves can also provide terminal insulation and strain relief. Suitable for a wide variety of applications, including
aerospace, military and rail applications. Sleeves meet the material and performance requirements of SAE-AMS-DTL-23053/5 Class 1. |
| PRINT METHOD / RIBBON: |
Thermal transfer: T312M-PRINTER, 1966-RIBBON
T212M-PRINTER, T200-RIBBON-1966 |
| SERVICE TEMPERATURE: |
-55°C to +135°C (-67°F to +275°F). |
| MINIMUM SHRINK TEMPERATURE: |
85°C (185°F) |
| COLOURS: |
White or yellow as standard. Other colors available on request with MOQ conditions. |
| AGENCY APPROVALS: |
UL recognised Standard 224 (File E35586); CSA certified (File 31929). |
| TENSILE STRENGTH: |
10.3MPa maximum (SAE-AMS-DTL-23053/5). |
| ULTIMATE ELONGATION: |
200% minimum (SAE-AMS-DTL-23053/5). |
| 2% SECANT MODULUS: |
172.4MPa maximum (SAE-AMS-DTL-23053/5). |
| LONGITUDINAL CHANGE: |
-20% maximum (SAE-AMS-DTL-23053/5). |
| HEAT AGEING: |
100% UE retained and print legible after 168 hours at 175°C (347°F). |
| HEAT SHOCK: |
No cracking, dripping for flowing and print legible after 4 hours at 250°C (482°F). |
| LOW TEMP. FLEXIBILITY: |
No cracking after 4 hours at -55°C (-67°F), 11mm (7/16 inch) mandrel bend. |
| MOULD GROWTH: |
Print legible after 56 day incubation (ISO 846B) - tensile strength and ultimate elongation maintained after testing. |
| FLAMMABILITY: |
UL rated, tubing flame tested. Burn time 60 seconds max. (ASTM D2671 Procedure B). |
| WATER ABSORPTION: |
0.5% maximum (ASTM D570). |
| COPPER MIRROR CORROSION: |
Non-corrosive; no piting or blackening of mirror after 16 hours at 175°C (347°F). (SAE-AMS-MIL-23053/5) |
| DIELECTRIC STRENGTH: |
19.7MV/m minimum (ASTM D2671). |
PRINT PERMANENCE:
-ADHERENCE
-FLUID RESISTANCE |
Meets the requirements of SAE AS5942 (20 rubs).
Meets the requirements of MIL-STD-202F method 215J. |
FLUID RESISTANCE,
Additional: |
|
THREAT
(*indicates thermal transfer
printing with 1966 ribbon only) |
TEST |
EFFECT |
| MIL-L-7808 lubricating oil |
SAE AS5942
(24 hours at 24°C (75°F), 20 rubs) |
Print legible |
| MIL-L-23699 lubricating oil |
SAE AS5942
(24 hours at 24°C (75°F), 20 rubs) |
Print legible |
| MIL-H-5606 hydraulic fluid |
SAE AS5942
(24 hours at 24°C (75°F), 20 rubs) |
Print legible |
MIL-T-83133 aircraft fuel (JP-8)
10W-40 (SAE J 183, SAE J300) |
SAE AS5942
(24 hours at 24°C (75°F), 20 rubs) |
Print legible |
Aviation gasoline (100/30)
SAE J 1703 |
SAE AS5942
(24 hours at 24°C (75°F), 20 rubs) |
Print legible |
| Skydrol™ 500 hydraulic fluid |
SAE AS5942
(24 hours at 24°C (75°F), 20 rubs) |
Print legible |
| 5% salt water (A-A-694) |
SAE AS5942
(24 hours at 24°C (75°F), 20 rubs) |
Print legible |
| MIL-A-8243 anti-icing fluid |
SAE AS5942
(24 hours at 24°C (75°F), 20 rubs) |
Print legible |
