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GLENAIR, INC. |
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8546.90.0000
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AIRCRAFT, HERCULES C-130,ASSAULT BREACHER VE,CARRIER, PERS M-113A1, M-113A2, M-113A3,TANK, ABRAMS M-1,RECOVERY VEHICLE, FU,ENGINE, AIRCRAFT T-58,SUPPORT EQUIPMENT, F-16 AIRCRAFT,LIGHT ARMORED VEHIC (TAMCN: E09467B),LIGHT ARMORED VEHIC (TAMCN: E09477M),LIGHT ARMORED VEHIC (TAMCN: E09487B),LIGHT ARMORED VEHIC (TAMCN: E09497M),LIGHT ARMORED VEHIC (TAMCN: E09507B),CONSOL PSE,LOW ALTITUTE NAVIGATION & TARGETING INFRARED SYSTEM(LANTIRN),INFANTRY CARRIER (STRYKER FIGHTNING VEHICLE),CONSOLIDATED GROUND SUPPORT EQUIPMENT,LAV, ANTI-TANK |
| NOT ESTABLISHED |
| -55.0 DEG CELSIUS AND 125.0 DEG CELSIUS |
| SOLVENT RESISTANT |
| 0.780 INCHES NOMINAL AFTER UNRESTRICTED RECOVERY |
| 0.520 INCHES NOMINAL AFTER UNRESTRICTED RECOVERY |
| 0.520 INCHES NOMINAL AFTER UNRESTRICTED RECOVERY |
| 1.600 INCHES NOMINAL AFTER UNRESTRICTED RECOVERY |
| 0.040 INCHES NOMINAL AFTER UNRESTRICTED RECOVERY |
| 0.040 INCHES NOMINAL AFTER UNRESTRICTED RECOVERY |
| 0.040 INCHES NOMINAL AFTER UNRESTRICTED RECOVERY |
| 1.600 INCHES NOMINAL AFTER UNRESTRICTED RECOVERY |
| 1000 POUNDS PER SQUARE INCH |
| MATERIAL OPTIONS: HEAT SHRINKABLE ELASTOMERIC POLYMER BLEND, MODIFIED, CROSSLINKED; MUST MEET REQUIREMENTS OF SPEC-01417-SC-X15112; CONTINUOUS OPERATING TEMPERATURE RANGE: -67 DEGREES FAHRENHEIT AND +257 DEGREES FAHRENHEIT; 2ND MATERIAL OPTION: VITON POLYMER BLEND, FLAME RESISTANT, FLEXIBLE, HEAT SHRINKABLE; CONTINOUS OPERATING TEMPERATURE RANGE: -94 DEGREES FAHRENHEIT TO 302 DEGREES FAHRENHEIT PER SPEC 01417-SC-X1511; 3RD MATERIAL OPTION: THERMOFIT FLUOROPOLYMER, MODIFIED, RADIATION CROSSLINKED, FLEXIBLE, ABRASION RESISTANT, FLAME RETARDED, HEAT SHRINKABLE PER SPECIFICATION RT-1334 |
| FLEXIBLE |
| TAN |
| PLASTIC POLYVINYL CHLORIDE |
| B7 TRANSITION-Y |
| 96906-MIL-STD-100 GOVERNMENT STANDARD AND 80204-ANSI Y14.5M-1982 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD |
