GORE® Umbilical Assemblies


Guaranteed 100 store releases on every umbilical assembly

GORE® Umbilical Assemblies are proven on many of today’s airborne platforms including A10 Warthog, F-16, Eurofighter, Harrier GR.9, and Tornado GR4 to name but a few.  Introduced to NATO in the mid 1990's, Gore identified a need to provide the market with a reliable, easy-to-use umbilical assembly that did not fail when used.



Features & Benefits

  • Incorporating FRCS- Field Replaceable Connector System
  • Jam-free push on/pull off connection
  • Flexibility for optimized routing
  • Proven flex-life in excess of 100,000 flexes
  • Qualified and currently in service
  • Ease of Installation
  • Reduce downtime/ increase aircraft availability

This video, provided by Lockheed Martin, demonstrates the jam-free store release offered by GORE® umbilical assemblies.

Gore Heritage in Defense and Aerospace

Specified for use on many of today’s platforms, Gore’s products for Airborne and Space Flight applications play a vital role in system performance providing significant reductions in overall program risk. For nearly 40 years Gore has been supplying products to the defense and space flight industries. Gore’s ability to provide solutions for complex packaging and routing constraints has resulted in a number of high performance products being selected for the Joint Strike Fighter, F-35 Lightning II, program.

Product Details

Gore manufactures hybrid round-cable assemblies to meet the international requirements of MIL-STD-1760 Aircraft/Store Electrical Interconnection System.

The standard provides a common electrical interface for the operation and employment of stores on aircraft and defines a complex arrangement of interfacing signals.

This interface standard defines a signal set containing power supplies, MIL-STD-1553B data buses, high and low bandwidth lines, and safety-critical discretes, and makes provision for the use of fiber-optic interfaces. The physical location and connector type/orientation is also standardized to foster interoperability of stores between different platforms. Connector options include MIL-DTL-38999/31 and FRCS.

Class I, Class II, or custom versions can be manufactured to meet any aircraft-integration requirements.

Gore's cable assembly uses highly flexible materials, specifically designed to be accommodated within the limited space of aircraft pylons.

Tests Performed

GORE® Cables have undergone the following tests:

Production tests

Continuity

MIL-STD-202F, Method 303

Insulation resistance/dielectric strength

MIL-STD-202F, Method 302 and 301

Electromagnetic compatibility (EMC)

IEC 96-1, Amendment 2

 

Thermal and dynamic tests

Rain and slush

MIL-STD-810B, Method 506

Icing

BS 3G 100 Part 2, Section 3, Sub-section 3.9, Test C

Vibration

MIL-STD-810B, Method 514.1, Figure 514.1-2, Curve D

Gunfire vibration

MIL-STD-810D, Method 519.3

Acoustic noise

MIL-STD-810D, Method 515.3, Section II, Category C

Mechanical shock

MIL-STD-810B, Method 516.1, Figure 516.1-1

Temperature shock

Based on MIL-STD-810B, Method 503

Temperature cycling

Based on MIL-STD-810B, Method 501, Procedure II and 502

Explosive atmosphere

Pan SP-P-90033, Paragraph 6.10.2, Issue 7

Humidity

MIL-STD-810B, Method 507, Procedure II

Solar radiation

MIL-STD-810B, Method 505

Flammability

UL 1581

Resistance to abrasion by scraping

SP-P-99301-00P

 

Chemical tests

Fungus

MIL-STD-810B, Method 508

Salt fog

MIL-STD-810B, Method 509

Contamination

Based on DEFENSE STANDARD 00-35, Part 3/3,
Chapter 4-04

Sand and dust

Based on MIL-STD-810B, Method 510 and Method 510.2 Procedure II

Mechanical Tests

GORE® MIL-STD-1760 cables have undergone an installation simulation, 1,000 cycle flex test at a rate of 15 cycles/minute (500 cycles in the X-axis followed by 500 cycles in the Y-axis). The term cycle refers to bending the harness directly at the rear of the connector from zero to +90 degrees, back through zero to  -90 degrees, and returning to zero, and is performed on both ends of the harness at temperatures from -20°C to +60°C. The test is based on MIL-STD-810B, Method 501, Procedure II and 502 to prove that the assembly can withstand repeated flexing without mechanical or electrical failure.  Additional testing to establish cable limitations achieved a proven flex-life in excess of 100,000 flexes.

Ease of Installation

GORE® MIL-STD-1760 cables can be attached to and removed from the ASI and MSI while operating in an NBC environment, in accordance with MIL-STD-1472, Paragraph 4.10. The technology enables fast and easy connector system replacement while maintaining proven product performance in excess of 100,000 flexes.

For more information about GORE® Umbilical Assemblies Contact Us.