Data Quality82%
MASS(Military Archive Scoring System)
ⓘ Regardless of era, the same scoring system applies to all units in the land-attack cruise missiles (lacm) category.
01 / Overview
AIST
💰 PERFORMANCE / PRICE ASSESSMENT Methodology ↗
LAND-ATTACK CRUISE MISSILES (LACM)
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PERFORMANCE/PRICE
70
UNIT COST (2025 USD)
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ⓘ Performance/Price and MASS score are computed across all units in the land-attack cruise missiles (lacm) category, regardless of era.
02 / Specs & Design
◎General5MOD.5
- Missile Typecruise missile
- DesignerState Military Industrial Committee
- Length1.1 m
- Diameter0 mm
- Launch Weight1,500 kg
◈Guidance5MOD.5
- Guidance TypeInertial / GPS
- Fire-and-ForgetYes
- Top-Attack CapableNo
- Inertial / GPS GuidanceYes
- Sea-SkimmingNo
▣Propulsion5MOD.5
- Propulsion Typeturbofan
- Motor TypeMS-400
- Boost StageYes
- Two-StageYes
- Fuel / Propellantkerosene
◇Performance5MOD.5
- Maximum Range500 km
- Top Speed250 m/s
- Top Speed (Mach)0.73 Mach
- Flight Profilesubsonic
- HypersonicNo
◆Warhead1MOD.1
- Warhead Weight350 kg
▤Launch Platform6MOD.6
- Launch PlatformPolonez MLRS
- Air-LaunchedNo
- Ground-LaunchedYes
- Naval-LaunchedNo
- Man-PortableNo
- Launcher TypeMLRS
⬢Production1MOD.1
- Operators1
03 / History
05 / MASS Score
LAND-ATTACK CRUISE MISSILES (LACM) RANKING Land-Attack Cruise Missiles (LACM)
MASS RANKINGSMASS ↗
38LAND-ATTACK CRUISE MISSILES (LACM)16BELARUS · ALL WEAPONS22PERFORMANCE/PRICE · LAND-ATTACK CRUISE MISSILES (LACM)
ⓘ Rankings are within theLand-Attack Cruise Missiles (LACM)category.
📖 TERMS ON THIS PAGE6terms
The initial propulsion phase where a high-thrust motor accelerates the missile to operational velocity.
Fire-and-forget refers to a missile guidance system where the missile guides itself to its target after launch, requiring no further input from the operator.
Launched from a ground-based platform, such as a vehicle or tripod, rather than an aircraft or other airborne system.
Guidance system combining inertial navigation (self-contained motion tracking) with GPS (satellite-based positioning) for precise trajectory correction in ballistic missiles.
A guidance method that uses inertial navigation sensors together with satellite‑based GPS signals to determine a missile’s position and steer it toward a target.
A two-stage ATGM propulsion system where a booster stage initially accelerates the missile before a sustainer stage maintains flight velocity.
These terms are listed automatically because they appear on this page.full encyclopedia →
📚 Sources