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Антон Бородин · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
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At a glance
Kh-22larger figure on 1 of 1
Kh-69larger figure on 0 of 1
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Configuration
| Specification | Kh-22 | Kh-69 |
|---|---|---|
| Type | Anti-ship cruise missile Air-to-surface missile[source] | Air-launched cruise missile[source] |
| Place of origin | Soviet Union[source] | Russia[source] |
| In service | 1968-present[source] | 2023–current[source] |
| Used by | Russia[source] | Russia[source] |
Wingspan
Single source300 cm (120 in)[source]
Warhead weight
Single source300 kg (660 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Wars | Russo-Ukrainian War Russo-Ukrainian war[source] | Russo-Ukrainian War[source] |
|---|
| Designer | MKB Raduga[source] | MKB Raduga[source] |
|---|
| Unit cost | $1 million[source] | — |
|---|
| Produced | 1962[source] | — |
|---|
| Warhead | 1,000 kg (2,205 lb) RDX or 350–1,000 kt (1.5–4.2 PJ) thermonuclear weapon[source] | — |
|---|
| Engine | R-201 liquid-fuel rocket[source] | TURBOFAN[source] |
|---|
| Propellant | Tonka-250 and IRFNA[source] | — |
|---|
| Flight ceiling | 10–14 km (33,000–46,000 ft) or 27 km (89,000 ft)[source] | — |
|---|
| Guidance system | Inertial guidance followed by terminal active radar homing[source] | GNSS , INS and Contrast seeker[source] |
|---|
| Accuracy | >300 ft (91 m) (CEP)[source] | — |
|---|
| Launch platform | Tu-22M, Тu-22К, Тu-95К22[source] | Su-30MK, Su-34, Su-35, Su-57, MiG-29K, MiG-35[source] |
|---|
| Manufacturer | MKB Raduga[source] | Tactical Missiles Corporation[source] |
|---|
| Role | — | Russian stealth subsonic air-launched cruise missile[source] |
|---|
| Source measurement | — | The Kh-69 ( Cyrillic : Х -69) (NATO reporting name: AS-22 'Kazoo' ) is a Russian stealth subsonic air-launched cruise missile . It was developed from the Kh-59 missile, and has a range of at least 400 km (250 mi). It has a reduced radar signature compared to its forerunners.[source]Kh-69 · Lead; only the objects and conditions stated in this passage The missile is reported to weigh under 800 kg (1,800 lb) and is reported to cruise at speeds of up to 1,000 km/h (620 mph). It can use either a cluster or a penetration warhead, weighing around 300 kilograms (660 lb).[source]Kh-69 · Technical characteristics; only the objects and conditions stated in this passage The Kh-69 uses GPS and GLONASS for guidance, with inertial backup. The missile is reportedly able to fly at an altitude as low as 20 meters above ground level , which greatly contributes to its low radar observability. An electro-optical seeker was reported in 2022 to round out the sensor suite.[source]Kh-69 · Technical characteristics; only the objects and conditions stated in this passage |
|---|
| Reported operators |
| — |
|---|