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In the realm of ultra-high-current switching, where system integrity and safety are paramount, specifications are not merely numbers—they are the definitive blueprint for performance under extreme stress. The B3T1-250.0 Military Metal Relay (complete designation: 80-3601 B-D2-C1-G-H 250A 80V) stands as a benchmark for 250-ampere DC power control in mission-critical applications. This comprehensive technical reference decodes its complete specification sheet, providing procurement engineers and system architects with the granular data needed to confidently integrate this powerhouse into Aircraft Engine start systems, heavy-duty Industrial Power distribution, and next-generation Military Aviation platforms.

Understanding the complete part number is the first step to mastering its specifications. The designation 80-3601 B-D2-C1-G-H is a structured code revealing its pedigree and core attributes.
The following parameters define the operational and safety envelope of the B3T1-250.0, distinguishing it from commercial-grade Industrial Power Relays.
| Parameter | Specification (B3T1-250.0 Typical) | Engineering Impact & Test Standard Reference |
|---|---|---|
| Rated Operational Voltage (Ue) | 80 V DC | Maximum design voltage. Dielectric strength and contact gap are engineered for this level. Basis for all dielectric tests. |
| Rated Conventional Free-Air Thermal Current (Ith) | 250 A | The current the relay can carry continuously with contacts closed in free air at 40°C ambient without exceeding temperature rise limits (typically ΔT ≤ 65K). Verified per MIL-STD-202. |
| Rated Making Capacity (Icm) | 750 A (3 x Ith) @ 80V DC, L/R ≤ 10ms | The maximum current the relay can close onto without contact weld or catastrophic failure. Critical for connecting to live battery banks or capacitive loads in New Energy systems. |
| Rated Breaking Capacity (Icn) | 375 A (1.5 x Ith) @ 80V DC, L/R ≤ 10ms | The maximum fault current the relay can safely interrupt. Defines its role in circuit protection. Validated with specialized high-power test circuits. |
| Maximum Contact Resistance (Initial) | ≤ 0.08 mΩ (80 µΩ) | Extremely low resistance is critical to minimize power loss (P=I²R). At 250A, even 100µΩ results in 6.25W of heat. Measured with 4-wire milliohm method per a specified test current (e.g., 10A). |
| Contact Material | Silver-Tungsten (AgW) or Silver-Tin Oxide (AgSnO2) | Chosen for high arc erosion resistance, anti-welding properties, and stable resistance over life. Far superior to materials in standard Automotive Relays. |
| Parameter | Typical Value | Design Consideration |
|---|---|---|
| Nominal Coil Voltage (Uc) | 28 V DC (Standard) | Matches 28VDC aircraft and military vehicle systems. Other voltages (e.g., 12V, 24V, 110V DC) available. |
| Coil Resistance @ 20°C | ~4.5 Ω ±10% | Results in a nominal pull-in current of ~6.2A and power of ~175W. Driver circuit must be robust. |
| Must Operate Voltage (Uop.min) | ≤ 20.0 V DC | Guaranteed pull-in under worst-case conditions (cold temperature, low line voltage). |
| Must Release Voltage (Ure.max) | ≥ 3.0 V DC | Ensures positive dropout when de-energized. |
| Maximum Continuous Coil Voltage | 32.0 V DC | Absolute limit to prevent insulation breakdown and overheating. |
These specs ensure physical survivability and define operational lifespan, key for OEM/ODM Manufacturers calculating total cost of ownership.
The demand is shifting from simple datasheet limits to comprehensive, traceable performance data. Leading-edge manufacturers provide statistical performance distributions (e.g., contact resistance S-curves, operate time histograms) and are developing digital twins of components like the B3T1-250.0. These virtual models, fed with real test data, allow system engineers to simulate performance under unique load profiles or environmental sequences before physical integration, reducing program risk for complex Military Aviation or Train propulsion projects.
Guaranteeing that every B3T1-250.0 meets its rigorous specifications requires a fusion of heavy industry capability and aerospace precision. Within our 500,000 sq.m. mega-facility, the production of this relay is a showcase of advanced manufacturing. We employ electron-beam welding for critical joints to ensure strength and consistent thermal properties. Each relay's contact alignment and pressure are set by robotic systems with force feedback, ensuring the critical ≤ 0.08 mΩ resistance spec is consistently achieved. This process-centric approach is the foundation of our High Quality Aviation and defense manufacturing philosophy.
The Breaking Capacity (Icn) specification is directly enabled by our R&D team's work in computational magnetics. Using 3D finite element analysis (FEA), they have optimized the geometry and strength of the permanent magnet blow-out system. This simulation-led design ensures the magnetic field strength is precisely calibrated to stretch and cool the 250A DC arc rapidly across the arc chutes, enabling it to meet and exceed the 375A breaking specification reliably, a technology that also informs our designs for Solid State Relay for Drone protection circuits.
Correct implementation is critical to realizing the specified performance in the field.
The B3T1-250.0's specifications are validated against a hierarchy of demanding standards, providing multiple layers of assurance:
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