Kh-38 | |
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Kh-38ME | |
Type | Tactical air-to-surface missile |
Place of origin | Russia |
Service history | |
Used by | Russia |
Production history | |
Manufacturer | Tactical Missiles Corporation JSC |
Specifications | |
Mass | 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) |
Maximum speed | Mach 2.2 |
Guidance system | Laser, active radar, IR, satellite, depending on variant |
Launch platform | Su-34, PAK FA |
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[]
- Kh-38MAE - inertial, active radar homing
- Kh-38MKE - inertial, satellite guidance
- Kh-38MLE - inertial, laser guidance
- Kh-38MTE - inertial, infrared guidance
See also[]
References[]
- ↑ 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[]
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The original article can be found at Kh-38 and the edit history here.