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At a glance
Kh-38larger figure on 4 of 4
TY-90larger figure on 0 of 4
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source4.2 m (13 ft 9 in)[source]
Length
Single sourceConfiguration
| Specification | Kh-38 | TY-90 |
|---|---|---|
| Speed | Mach 2.2[source] | > Mach 2[source] > Mach 2[source] |
| Type | Tactical air-to-surface missile[source] | Air-to-air & surface-to-air missiles[source] |
| Place of origin | Russia[source] | China[source] |
| In service | 2012 (Kh-38ME) 2019 (Kh-36)[source] |
1.95 meter[source]
up to
Single sourceup to 250 kg (551 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
1990’s – present[source] |
| Used by | Russia[source] | China[source] |
|---|
| Wars | Syrian Civil War Russo-Ukrainian War[source] | — |
|---|
| Designer | Tactical Missiles Corporation JSC[source] | — |
|---|
| Designed | 2007 (Kh-38ME) - 2015 (Kh-36)[source] | — |
|---|
| Manufacturer | Tactical Missiles Corporation JSC[source] | China Aviation Industry Corporation I[source] |
|---|
| Produced | 2015 (Kh-38M) - 2019 (Kh-36)[source] | since 1990s[source] |
|---|
| Warhead | HE fragmentation, cluster warhead, armor-piercing[source] | 3 kg warhead[source] |
|---|
| Detonation mechanism | Contact fuse[source] | impact / proximity[source] |
|---|
| Engine | Two-stage solid rocket motor[source] | Solid-fuel rocket motor[source] |
|---|
| Flight altitude | 200-12000 m[source] | 0 – 6 km[source] |
|---|
| Guidance system | Laser, active radar, IR, satellite, depending on variant[source] | ImIR IR[source] |
|---|
| Launch platform | Kh-38: Su-34 , Su-25SM3 , Su-57 , Ka-52K , MiG-29K Kh-36: Su-57 , MiG-35[source] | Air & surface[source] |
|---|
| Role | family of standoff air-to-surface missiles meant to succeed the Kh-25 and Kh-29 missile families[source] | — |
|---|
| Source measurement | The Kh-38/Kh-38M ( Russian : Х -38 ) is a family of standoff air-to-surface missiles meant to succeed the Kh-25 and Kh-29 missile families. The Kh-38 also serves as the basis for the Kh-36 unpowered and powered glide-bombs.[source]Kh-38 · Lead; only the objects and conditions stated in this passage The basic configuration of the Kh-38M was revealed at the 2007 Moscow Air Show (MAKS) . The first prototypes of the missile had initially folding wings and tail fins for internal carriage, and would have a variety of seeker heads for different variants. Different warheads (fragmentation, cluster munitions , penetrating) can also be fitted. The Kh-38M is meant to succeed the Kh-25 and Kh-29 missile families. It can be used by combat aircraft such as the Sukhoi Su-34 and Sukhoi Su-57 , and it is planned to be integrated on the Kamov Ka-52 K helicopter. The first test firing took place in 2010 from a Su-34, and production was ordered to start in 2015.[source]Kh-38 · Design and development; only the objects and conditions stated in this passage The Kh-38M was first used in combat during the Russian military intervention in the Syrian civil war . It was also used during the 2022 invasion of Ukraine .[source]Kh-38 · Operational history; only the objects and conditions stated in this passage Kh-36 Grom-E1 - Rocket assisted version of the Grom-E2. Sometimes referred as a hybrid missile glide bomb. AS-23 tactical cruise missile derivative/AGM with 120 km range[source]Kh-38 · Variants / Kh-36; only the objects and conditions stated in this passage Kh-36 Grom-E2 - AS-23B/KAB-type guided glide bomb with 50 km range.[source]Kh-38 · Variants / Kh-36; only the objects and conditions stated in this passage Both versions of the Grom are of 600 kg weight, with various guidance mechanisms, and both are created on the basis of the Kh-38M short-range tactical missile and also have modular structures, warheads and seekers. This weapon was first seen at MAKS 2015, and intended to equip all types of fighters, including the MiG-35 and Su-57 .[source]Kh-38 · Variants / Kh-36; only the objects and conditions stated in this passage | — |
|---|
| Propellant | — | Solid fuel[source] |
|---|
| Flight ceiling | — | 6 km[source] |
|---|
| guidance | — | infrared homing[source] |
|---|