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Rolls-Royce Power Systems (mtu)
MTU MB 873 Ka-501
V12 twin-turbocharged diesel that has powered every production Leopard 2 variant since 1979, tracing its design back to the cancelled US/German MBT-70 program. Built under the mtu brand by Rolls-Royce Power Systems, distinct from Munich-based MTU Aero Engines.
In service since 1979
Compiled from public sources ·primary reference ↗
1,500
hp
2,200
kg
Procurement snapshot
Availability & export
German export-licensed
BAFA licensing with strict end-use review; approvals can be politically constrained.
Channel: Direct commercial / G2G
Fielded & proven
Operator data not public
In service since 1979. Status: active.
Lifecycle cost (est.)
No public unit price to model from. Why so few systems publish one →
Interoperability
No standardised NATO calibre / datalink detected in public specs.
Competitive field
13 comparable systems from 9 other manufacturers
Counted in the WeaponSpecs database: engines built by another manufacturer. A count of what this catalog holds, not a survey of the whole market. See the alternatives →
Derived guidance from public data, export regime by country of origin, lifecycle from the GAO ~30% acquisition rule. Verify eligibility, pricing and offsets with the manufacturer and your acquisition authority.
Overview
The MB 873 Ka-501 displaces about 47.6 liters (170 mm bore x 175 mm stroke) and produces roughly 1,100 kW (1,500 hp) at 2,600 rpm with peak torque near 4,700 N-m. Rolls-Royce Power Systems won a new order for 300 MB 873 engines for further Leopard 2 production in 2025. This record covers the bare engine; published weight figures for the combined EuroPowerPack (engine plus transmission and cooling), roughly 1,800 kg, are not the engine's standalone weight and are omitted here rather than misattributed.
Powers these platforms
Systems in the WeaponSpecs database that list the MTU MB 873 Ka-501 as their engine.
Full specifications
Physical
Dimensions, weight and crew.
| Length Overall length including gun/probe where applicable. | 1.8 m |
|---|---|
| Width Overall width, matters for rail/road transport of vehicles. | 1.98 m |
| Height Overall height. Lower profile is harder to spot and hit for ground vehicles. | 1.03 m |
| Empty weight Weight without fuel, ammunition or crew. | 2,200 kg |
Propulsion
Engine, power and fuel.
| Engine power Engine output power. Higher moves more weight faster. | 1,500 hp |
|---|---|
| Propulsion type Turbofan, turboshaft, diesel, gas turbine, solid-fuel rocket, ramjet… | V12 twin-turbocharged diesel |
Specifications compiled from public Rolls-Royce Power Systems (mtu) and reference sources ↗. Published defense figures are approximations, treat comparisons as directional. Last verified 2026-08-10.
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