Kh-38MTE
Kh-38MTE
Standoff Weapons
Basic Information
Name
Kh-38MTE
Designation
Kh-38MTE
Alternate Designation
—
Equipment Type
Standoff Weapons
Manufacturer
Tactical Missiles Corporation (KTRV)
Date of Introduction
2012
Description
The Kh-38MTE standoff weapon variant features an infrared (IR) imaging camera combined with automatic inertial navigation along with either a High Explosive (HE) fragmentation or penetrating warhead. The missile can be released from an altitude of 200 to 12,000 meters and an airspeed between 15 and 450 meters per second. After launch the missile can turn up to +/- 80-degree (right/left) in the horizontal plane to engage its intended target with a hit probability between 60 to 80 percent.
Ground Specifications
Max Speed
2716.6 km/h
Range
40.0 km
Overview (Deagel)
Group
Standoff Weapons
Status
Active
Origin
Russia
Contractor
Tactical Missiles Corporation (KTRV)
Initial Operational Capability (IOC)
2012
Total Production
?
Specifications (Deagel)
Dimensions — Diameter
310 millimeter
Dimensions — Length
4.2 meter
Dimensions — Wingspan
1.1 meter
Mass — Warhead
250 kilogram
Mass — Weight
520 kilogram
Percentage — Hit Probability
80 %
Performance — Max Launch Altitude
12,000 meter
Performance — Max Range
40 kilometer
Performance — Min Launch Altitude
200 meter
Performance — Min Range
3 kilometer
Speed — Max Launch Airspeed
450 mps
Speed — Min Launch Airspeed
15 mps
Speed — Top Speed
2.2 mach
Time — Service Life
10 year
Variants
Variant 1
Kh-38MLE
Variant 2
Kh-38MAE
Variant 3
Kh-38MTE
Variant 4
Kh-38MKE
Details
Country of Origin
Russia
Sources
deagel.com: https://www.deagel.com/x/x/a002425
Classification
Domain
Ground
Equipment Status
Active
Dimensions
Length
4.2 m
Width
—
Height
—
Weight
520 kg
Operators (2)
Russia
Egypt
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