ACruise & anti-ship missiles
Hyunmoo-3
Long-range, all-weather cruise missile Land-attack missile Surface-to-surface missile Submarine-launched cruise missile
FORCETALLY
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ACruise & anti-ship missiles
Long-range, all-weather cruise missile Land-attack missile Surface-to-surface missile Submarine-launched cruise missile
At a glance
Hyunmoo-3larger figure on 0 of 1
Kh-22larger figure on 1 of 1
Measured figures
3A
Single source19 feet (5.8 m) (3A)[source]
Length
Single sourceConfiguration
| Specification | Hyunmoo-3 | Kh-22 |
|---|---|---|
| Type | Long-range, all-weather cruise missile Land-attack missile Surface-to-surface missile Submarine-launched cruise missile[source] | Anti-ship cruise missile Air-to-surface missile[source] |
| Place of origin | South Korea[source] | Soviet Union[source] |
| In service | 2006–present (3A) 2009–present (3B) 2012–present (3C)[source] | 1968-present[source] |
| Used by | Republic of Korea Army Republic of Korea Navy[source] | Russia |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
11.65 m (38.2 ft)[source]
Operational; Hyunmoo-3A
Single sourceOperational; Hyunmoo-3B
Single sourceOperational; Hyunmoo-3C
Single sourceOperational; Hyunmoo-3D
Single sourceHyunmoo-3A - 500 kilometers (310 mi) Hyunmoo-3B - 1,000 kilometers (620 mi) Hyunmoo-3C - 1,500 kilometers (930 mi) Hyunmoo-3D - 3,000 kilometers (1,900 mi)[source]
Operational; Kh-22M/MA
Single source600 km (320 nmi) (Kh-22M/MA)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designer | Agency for Defense Development LIG Nex1[source] | MKB Raduga[source] |
|---|
| Manufacturer | LIG Defense & Aerospace[source] | MKB Raduga[source] |
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| Variants | Hyunmoo-3A Hyunmoo-3B Hyunmoo-3C Hyunmoo-3D[source] | — |
|---|
| Warhead | Conventional: 500 kilograms (1,100 lb) conventional explosive[source] | 1,000 kg (2,205 lb) RDX or 350–1,000 kt (1.5–4.2 PJ) thermonuclear weapon[source] |
|---|
| Engine | Samsung Hanwha Techwin (or Daewoo Doosan) (SSM-760K ?) turbofan[source] | R-201 liquid-fuel rocket[source] |
|---|
| Guidance system | INS , GPS , Terrain Contour Matching[source] | Inertial guidance followed by terminal active radar homing[source] |
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| Wars | — | Russo-Ukrainian War Russo-Ukrainian war[source] |
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| Unit cost | — | $1 million[source] |
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| Produced | — | 1962[source] |
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| Propellant | — | Tonka-250 and IRFNA[source] |
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| Flight ceiling | — | 10–14 km (33,000–46,000 ft) or 27 km (89,000 ft)[source] |
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| Accuracy | — | >300 ft (91 m) (CEP)[source] |
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| Launch platform | — | Tu-22M, Тu-22К, Тu-95К22[source] |
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| Reported operators |
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