CONMOLY / ENGINEERING & CONNECTIVITY
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.
Specialty Products (Aerospace & Defense)
CM-SPECIAL-1760
MIL-STD-1760 Cables
Reference configurations only; specifications and certifications require confirmation.
Selection reference. Published third-party figures below describe specific reference configurations; they are not Conmoly guaranteed values or certifications. Confirm the final construction and test requirements with engineering.
Dimensions and bend radii vary slightly across Class I, Class I (FO) and Class II part numbers; the applicable range is shown.
Scroll the table horizontally to view all configuration conditions.
| Parameter | Reference value | Configuration / condition |
|---|---|---|
| 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 |
Reference source: www.gore.com
| 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 |
Standard and product names identify the target interface only and do not imply unverified compliance, qualification or platform approval.
Reference configuration: High-voltage power, data pairs and single-mode fiber are integrated into a low-mass, weatherproof, crush-resistant tether for continuous drone power and secure high-bandwidth communication.
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