FORCETALLY
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At a glance
Mark 46 torpedolarger figure on 0 of 4
VA-111 Shkvallarger figure on 4 of 4
Measured figures
Length
Single source8 ft 6 in (2.59 m )[source]
Length
Single sourceConfiguration
| Specification | Mark 46 torpedo | VA-111 Shkval |
|---|---|---|
| Type | Lightweight anti-submarine torpedo[source] | Supercavitating torpedo[source] |
| Place of origin | United States[source] | Soviet Union[source] |
| In service | • Mod 0: 1963 • Mod 5: 1979[source] | 1977–present[source] |
| Used by | See operators[source] | Russian Navy and Iranian Navy |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
8,200 mm (26 ft 11 in)[source]
Maximum; >
Single source>40 kn (74 km/h ; 46 mph )[source]
Maximum; Launch speed
Single sourceMaximum; Launch speed Maximum speed: in excess of
Single sourceMaximum; Maximum speed
Single sourceMaximum; Maximum speed or greater
Single sourceLaunch speed: 50 knots (93 km/h; 58 mph) Maximum speed: in excess of 200 knots (370 km/h; 230 mph)[source]
Launch speed: 50 knots (93 km/h; 58 mph) Maximum speed: 200 knots (370 km/h; 230 mph) or greater[source]
Operational; Operational range
Single source12,000 yd (11,000 m )[source]
Around (new version). Older versions only
Single sourceEffective; Effective firing range
Single sourceEffective; Shkval Shkval 2 : From
Single sourceRange
Single sourceShkval : 7 km (4.3 mi) Shkval 2 : From 11–15 km (6.8–9.3 mi)[source]
Around 11–15 km (6.8–9.3 mi) (new version). Older versions only 7 km (4.3 mi)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designer | Naval Ordnance Test Station Pasadena Aerojet Alliant Techsystems[source] | NII-24 research institute[source] |
|---|
| Designed | 1960[source] | 1960s–70s[source] |
|---|
| Manufacturer | Aerojet Naval Ordnance Station Forest Park Honeywell Raytheon[source] | Tactical Missiles Corporation[source] |
|---|
| Variants | Mod 0 Mod 1 Mod 2 Mod 5 Mod 5A Mod 5A(S) Mod 5A(SW)[source] | Shkval 2, Shkval-E[source] |
|---|
| Warhead | PBXN-103 high explosive (bulk charge)[source] | Conventional explosive or nuclear[source] |
|---|
| Engine | Two-speed, reciprocating external combustion[source] | Solid-fuel rocket[source] |
|---|
| Propellant | Otto fuel II[source] | Solid-fuel[source] |
|---|
| Maximum depth | >1,200 ft (370 m)[source] | — |
|---|
| Guidance system | Active or passive/active acoustic homing[source] | GOLIS autonomous inertial guidance[source] |
|---|
| Launch platform | Mark 32 Surface Vessel Torpedo Tubes , ASW Aircraft, RUM-139 VL-ASROC[source] | 533 mm (21 in) torpedo tubes[source] |
|---|
| Produced | — | 1977–present[source] |
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| Reported operators |
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