The termination region — where the cable transitions into the connector — concentrates more sources of electrical risk in less space than almost any other location in a high-voltage assembly. Many partial-discharge and dielectric failures originate here when field stress, material interfaces, trapped air, or mechanical strain are not explicitly controlled. The mechanisms are understood, and with the right engineering approach they are preventable.
Termination Engineering · 10 kV – 250 kV DC · Aerospace · Defense · Medical · Scientific
In connector and cable assembly practice, the term termination is used loosely to mean almost any junction — a contact crimp, a solder joint, even a connector mating interface. That usage creates confusion when discussing high-voltage failure modes, so it is worth being precise.
For the purposes of this note, termination design refers to the engineered transition zone between the cable insulation system and the connector body insulation — the region where the cable's dielectric structure ends and the connector's dielectric structure begins, including the conductor transition, shield cutback (if applicable), void elimination strategy, and strain relief geometry.
In power-cable termination practice, the termination must generally address four functions: provide electric stress control at the point of shield cutback, provide external leakage insulation appropriate to the environment, seal the cable end against the external environment, and mechanically support the conductor at the point of transition. IEEE Std 48-2020, which addresses AC terminations for shielded cables with laminated insulation rated 2.5 kV through 765 kV and extruded insulation rated 2.5 kV through 500 kV, provides test procedures and requirements in this context. Each of these four functions has a corresponding failure mode in practice.
Note on DC vs. AC Field Distribution
IEEE Std 48 and IEC 60840 address AC cable systems. For DC applications, the steady-state electric field distribution is governed primarily by the conductivity/resistivity of the dielectric materials rather than permittivity alone — which means that at elevated temperature, resistive grading can shift field distribution in ways that capacitive or geometric grading alone may not fully control. DC-rated connector assemblies above 10 kV require explicit analysis of the resistive field distribution across the operating temperature range. This is one reason that DC high-voltage design cannot be directly adapted from AC cable accessory practice.
Many high-voltage dielectric failures in termination regions share a common initiating mechanism: partial discharge (PD) in a void, gap, contamination path, or field concentration point within or adjacent to the insulation system at the termination region. The specific physical location varies by design and fabrication method, but the four most consequential origination sites are:
The most common method for insulating multi-conductor high-voltage terminations is to fill the backshell or termination cavity with a castable compound — silicone RTV, polyurethane, or epoxy — applied at atmospheric pressure. The difficulty is that complex termination geometries contain blind cavities, conductor bundles, and abrupt cross-section changes that trap air as the compound flows in. The compound cures around the trapped bubbles. Routine production inspection may not reliably detect these voids: visual inspection sees only the surface, and conventional X-ray may detect larger voids but can miss small voids, thin gaps, or interface defects depending on material contrast, geometry, and resolution.
At lower voltages, small air voids may not produce damaging partial discharge. As voltage increases into the high-voltage range — especially in compact connector geometries — air-filled voids in the termination region become a predictable PD risk unless the geometry, materials, pressure environment, and test margins are explicitly controlled. The dielectric strength of air at sea level is approximately 3 kV/mm; silicone rubber is 18–25 kV/mm depending on compound and geometry. A void concentrates the local field to well above the surrounding material's design stress. Partial discharge initiates in the void, erodes the adjacent solid insulation over time, and progresses to dielectric breakdown.
Hi-pot testing — applying a fixed DC or AC withstand voltage for a defined period — is a go/no-go screen. It confirms that the assembly does not fail at the test voltage at the moment of test. It does not detect incipient voids, marginal insulation, or latent PD that initiates below the test voltage threshold. For example, depending on geometry and void location, an assembly that passes a 50 kV hi-pot screen could still exhibit PD at a 30 kV operating voltage if small voids or interfacial gaps are present.
The technically correct screen for void-related failure is corona / partial discharge testing — measuring the voltage at which discharge activity initiates (the partial discharge inception voltage, or PDIV) and confirming that this threshold exceeds the rated operating voltage by an appropriate margin. This test requires instrumentation, fixturing, shielding, and environmental controls that are not part of ordinary low-voltage cable assembly production.
Common Misconception
Passing a hi-pot test does not confirm the absence of partial discharge at operating voltage. Hi-pot and partial discharge inception testing are complementary screens — they detect different failure conditions. An assembly can pass hi-pot and still exhibit PD at rated voltage if the PDIV is between the operating voltage and the hi-pot test voltage.
The dielectric strength of air is pressure-dependent. At sea level, air breaks down at approximately 3 kV/mm under uniform-field conditions. At 70,000 feet, ambient pressure is only a few percent of sea-level pressure — approximately 4–5% under a standard-atmosphere model — and the Paschen curve shows that breakdown voltage drops significantly at reduced pressure, reaching a minimum (the Paschen minimum) before rising again at very low pressures. For aircraft and aerospace systems operating at altitude or in depressurized enclosures, any air void that is electrically benign at sea level may become a PD site at altitude.
This is why the design target for aerospace high-voltage cable assemblies is to avoid air-filled voids in electrically stressed regions, minimize trapped gas in the dielectric path, and verify adequate PDIV margin under the relevant pressure environment — not simply to ensure that any voids present are small enough to be tolerable at ground level.
Most cable assembly procurement specifications define the cable, the connector, the termination length, and the electrical performance requirements — and leave the termination design to the manufacturer's discretion. A manufacturer without high-voltage engineering capability will apply a standard potting process, perform a hi-pot screen, and deliver an assembly that may or may not have the necessary field grading geometry at the shield cutback edge.
Field grading at the shield cutback — the controlled redistribution of field lines away from the abrupt shield edge — is not a feature that emerges automatically from assembly practice. It requires explicit engineering: geometric shaping of the insulation profile, selection of materials with defined permittivity relationships, or the application of stress-grading materials. These decisions must be made at the design stage, not the assembly stage.
The governing physics of the termination region is the same as elsewhere in a high-voltage system: the electric field concentrates at geometric discontinuities, at material boundaries where permittivity changes, and at any location where the conductor-to-ground distance decreases abruptly. What makes the termination region different is the density of these features in a small space.
In the cable body, the field distribution is well-defined: a coaxial geometry with radially symmetric field, calculable from first principles, with no material discontinuities in the dielectric path. In the termination region, the coaxial geometry ends, the conductor transitions in cross-section, the shield terminates, the cable insulation gives way to connector body insulation, and the geometry becomes three-dimensional and irregular. Each of these changes affects the field distribution, and their interactions are not amenable to simple analytical approximation.
This is the reason Caton performs electrostatic field modeling — using finite-element simulation tools — before any termination design goes to tooling. Field modeling makes the distribution visible, identifies concentration points, and allows evaluation of design changes before hardware is built. A termination design that looks adequate from dimensional inspection may still exhibit unacceptable field concentration at a specific geometric feature — and that feature will not become visible until either the simulation or a failure reveals it.
Engineering Note — Field Modeling
Caton uses Electro V10.2 for electrostatic field analysis of termination geometry prior to tooling. The analysis confirms that field intensity at all material interfaces and geometric transitions remains within the design margins for the insulation system selected. This step occurs before any prototype hardware is built — because fabrication and test are not cost-effective substitutes for geometry analysis.
The following questions separate suppliers with genuine high-voltage engineering capability from those applying standard cable assembly practice to a high-voltage application. A supplier that cannot answer these questions with specific design rationale, process controls, and test evidence may be treating a high-voltage termination as a conventional cable assembly problem.
References are provided to support the technical claims in this application note and to allow engineers to verify source material independently. Where standards are cited, the edition current at time of publication applies. Contact our engineering team with questions about how any reference applies to a specific application.