Kh-38

Kh-38

Kh-38ME
Type Tactical air-to-surface missile
Place of origin Russia
Service history
In service 2012
Used by Russia
Production history
Designer Tactical Missiles Corporation JSC
Designed 2007
Manufacturer Tactical Missiles Corporation JSC
Produced 2013
Specifications
Weight 520 kg (1,150 lb)
Length 4.2 m (13 ft 9 in)
Diameter 0.31 m (12.2 in)
Warhead HE fragmentation, cluster warhead, armor-piercing
Warhead weight up to 250 kg (551 lb)
Detonation
mechanism
Contact fuse

Engine Solid rocket motor
Wingspan 1.14 m (44.9 in)
Operational
range
up to 40 km (21.6 nmi)
Speed Mach 2.2
Guidance
system
Laser, active radar, IR, satellite, depending on variant
Launch
platform
Su-34, PAK FA, Ka-52K

The Kh-38/Kh-38M (Russian: Х-38) is a family of air-to-surface missiles meant to succeed the Kh-25 family of missiles.

Design

The basic configuration of the Kh-38M was revealed at the 2007 Moscow Air Show (MAKS). The modular guided air-to-surface missile is meant to succeed the venerable Kh-25 missile family. The missile is designed to be carried by the fifth-generation PAK FA fighter aircraft. The missile has folding wings and tail fins for internal carriage, and would have a variety of seeker heads for different variants.[1]

Variants

See also

References

  1. Barrie, Douglas and Komarov, Alexey. "War on Two Fronts for Russia's Missile Builders ". Aviation Week, 10 September 2007. Retrieved: 25 May 2014.

External links

This article is issued from Wikipedia - version of the 10/29/2016. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.