Conmoly | CM-SPECIAL-1760 | MIL-STD-1760 Umbilical Assemblies
Shenzhen Xinju New Materials Technology Co., Ltd.
https://conmoly.com

Selection reference; third-party published figures are not Conmoly guaranteed specifications or certifications. Final specifications require configuration review. Images illustrate product form.
Reference configuration: Sealed high-flex hybrid umbilicals for aircraft pylon and mission-store interfaces use controlled disconnect load, EMI shielding and long flex life for safe release and repeat maintenance.

Dimensions and bend radii vary slightly across Class I, Class I (FO) and Class II part numbers; the applicable range is shown.
Store releases: 100 guaranteed releases | Matched connector assembly system
Flex life: > 100,000 cycles | Class I / I(FO) / II
Manual disconnects: 500 cycles | Certification test condition
Shield coverage: > 85% | Silver-plated copper braid
Outer diameter: 18.3–18.7 mm | Class II through Class I
Static / dynamic bend radius: 45.8–46.8 / 91.5–93.5 mm | By part number
Temperature range: −60 to +150 °C | All standard part numbers
Source: https://www.gore.com/products/mil-std-1760-cables-umbilical-assemblies-defense-aircraft

Class I: Standard mission-interface assembly with multiple shell sizes and inserts.
Class I fiber type: Adds OM3 multimode fiber to the hybrid electrical construction.
Class II: Wire set and assembly defined to the applicable mission interface.
Functional units: Power, data, fiber, video and discrete units are separated by function.
Unit isolation: Twists, coax, individual shields and spacing manage coupling.
Strength or overall shield: Tensile load, return path and platform grounding determine the structure.
Sealed rugged cover: Resists fluids, abrasion, temperature, repeated deployment and mission loads.
Mission termination: Connectors, branches, marking, strain relief and rapid-service interfaces are integrated.
Interface document: Pinout, protocols, connector and standard revision
Power and signal: Voltage, current, bandwidth, optical path and shield zoning
Mechanical boundary: Length, diameter, mass, tensile load and bend radius
Mission environment: Temperature, fluids, abrasion, vibration, shock and sealing
Operation: Reel, release, mating, maintenance and storage cycles
Acceptance matrix: Electrical, mechanical, environmental and system tests

Pin-by-pin continuity, insulation, hipot and wire map
High-speed, fiber or RF unit performance
Tensile, flex, abrasion, sealing and termination retention
Interface-standard environment and system integration
Military-aircraft pylon stations
Weapon and mission-store interfaces
ASI/MSI rapid connection
Frequent maintenance and repeated release
Hybrid power, data and fiber construction
Mission connector, branch and strain relief
Fixed-length complete and serialized assembly
Standard and product names identify the target interface only and do not imply unverified compliance, qualification or platform approval.