R-74M2

Russian next-generation short-range infrared-homing air-to-air missile, an improved derivative of the R-73/R-74 family with a claimed high off-boresight capability.

Compiled from public sources ·primary reference ↗ ·last verified 2026-07-05

km range

2.5

Mach

kg warhead

Several performance figures for Russia-origin systems are manufacturer or state claims with limited independent verification. Treat these specs as directional, not tested values.

Procurement snapshot

Availability & export

Russian state channel

Rosoboronexport monopoly; Western sanctions exposure and payment/logistics risk for many buyers.

Channel: Rosoboronexport (state)

Fielded & proven

Operator data not public

Status: active.

Lifecycle cost (est.)

No public unit price to model from.

Interoperability

No standardised NATO calibre / datalink detected in public specs.

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.

Full specifications

Performance

Speed, range, altitude and engagement capability.

Max speed (Mach) Maximum speed as a multiple of the speed of sound. Mach 2+ is typical for air-superiority fighters.: 2.5 Mach

Stronger than 53% of missiles
Range Maximum distance: ferry range for aircraft, operational range for vehicles, maximum engagement distance for missiles. Higher means more standoff or persistence.: 40 km

Stronger than 36% of missiles

Firepower

Armament, payload and guidance.

Warhead Warhead mass. Heavier generally means larger effect radius, at the cost of range.: 8 kg

Stronger than 15% of missiles
Warhead type Blast-fragmentation, shaped charge (HEAT), penetrator, thermobaric or nuclear-capable.: High-explosive fragmentation
Guidance How the weapon finds its target: inertial, GPS/GLONASS, active/semi-active radar, infrared, laser, TV, wire.: Thermal imaging infrared seeker, LOAL (lock-on-after-launch), IRCCM

Propulsion

Engine, power and fuel.

Propulsion type Turbofan, turboshaft, diesel, gas turbine, solid-fuel rocket, ramjet…: Solid-fuel rocket

Specifications compiled from public Vympel NPO and reference sources ↗. Published defense figures are approximations, treat comparisons as directional. Last verified 2026-07-05.

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