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At a glance
Gabriel (missile)larger figure on 0 of 1
Kh-22larger figure on 1 of 1
Measured figures
A/S
Single sourceMark I
Single sourceConfiguration
| Specification | Gabriel (missile) | Kh-22 |
|---|---|---|
| Type | Anti-ship missile[source] | Anti-ship cruise missile Air-to-surface missile[source] |
| Place of origin | Israel[source] | Soviet Union[source] |
| In service | 1970[source] | 1968-present[source] |
| Used by | See operators[source] | Russia |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Mark II
Single sourceMark III Mark III
Single sourceMark IV
Single sourceMark V
Single sourceMark I: 3.35 m (11.0 ft) Mark II: 3.36 m (11.0 ft) Mark III: 3.75 m (12.3 ft) Mark III A/S: 3.78 m (12.4 ft) Mark IV: 4.7 m (15 ft) Mark V: 5.5 m (18 ft)[source]
Length
Single source11.65 m (38.2 ft)[source]
Wingspan
Single sourceMark I / II
Single sourceMark III Mark IIIA/S1.08 m (
Single sourceMark IV
Single sourceMark I / II:1.35 m (4 ft 5 in) Mark III:1.32 m (4 ft 4 in) Mark IIIA/S1.08 m (3 ft 7 in) Mark IV:1.60 m (5 ft 3 in)[source]
Wingspan
Single source300 cm (120 in)[source]
A/S
Single sourceMark I
Single sourceMark II
Single sourceMark III Mark III
Single sourceMark IV
Single sourceMark V
Single sourceMark I: 430 kg (950 lb ) Mark II: 522 kg (1,151 lb) Mark III: 560 kg (1,230 lb) Mark III A/S: 590 kg (1,300 lb) Mark IV: 960 kg (2,120 lb) Mark V: 1,250 kg (2,760 lb)[source]
Mass
Single source5,820 kg (12,800 lb)[source]
Operational; IIIA/S
Single sourceOperational; Mark I
Single sourceOperational; Mark II
Single sourceOperational; Mark III Mark
Single sourceOperational; Mark IV
Single sourceOperational; Mark V/Blue Spear/Sea Serpent
Single sourceMark I: 20 km (12 mi) Mark II:6–36 km (3.7–22.4 mi) Mark III:36 km (22 mi) Mark IIIA/S:60 km (37 mi) Mark IV:200 km (120 mi) Mark V/Blue Spear/Sea Serpent:400 km (250 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.
| Wars | Yom Kippur War[source] | Russo-Ukrainian War Russo-Ukrainian war[source] |
|---|
| Manufacturer | Israel Aerospace Industries[source] | MKB Raduga[source] |
|---|
| Unit cost | US$5 million per missile (Gabriel V / Blue Spear)[source] | $1 million[source] |
|---|
| Variants | developed from Luz (missile)[source] | — |
|---|
| Warhead | Mark II: 100 kg (220 lb) Mark III / IIIA/S: 150 kg (330 lb) Mark IV: 240 kg (530 lb)[source] | 1,000 kg (2,205 lb) RDX or 350–1,000 kt (1.5–4.2 PJ) thermonuclear weapon[source] |
|---|
| Flight altitude | 2.5 m (8 ft 2 in)[source] | — |
|---|
| Guidance system | Mark I / II:Semi-Active Radar Mark III / IIIA/S / IV: Active Radar, Mark V/ Blue Spear/ Sea Serpent: Inertial Navigation System (INS), Global Positioning System GPS, Active Radar Seeker, Two-way Data Link.[source] | Inertial guidance followed by terminal active radar homing[source] |
|---|
| Launch platform | Mark I-V: naval ships; Blue Spear: naval ships, Scania 6x6 or 8x8 truck-mounted.[source] | Tu-22M, Тu-22К, Тu-95К22[source] |
|---|
| Alternative designation | Gabriel[source] | — |
|---|
| Designer | — | MKB Raduga[source] |
|---|
| Produced | — | 1962[source] |
|---|
| Engine | — | R-201 liquid-fuel rocket[source] |
|---|
| Propellant | — | Tonka-250 and IRFNA[source] |
|---|
| Flight ceiling | — | 10–14 km (33,000–46,000 ft) or 27 km (89,000 ft)[source] |
|---|
| Accuracy | — | >300 ft (91 m) (CEP)[source] |
|---|
| Reported operators | — |
|
|---|