FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Torped 62larger figure on 0 of 3
VA-111 Shkvallarger figure on 3 of 3
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source5,990 mm (236 in)[source]
Length
Single sourceConfiguration
| Specification | Torped 62 | VA-111 Shkval |
|---|---|---|
| Type | Heavyweight torpedo[source] | Supercavitating torpedo[source] |
| Place of origin | Sweden[source] | Soviet Union[source] |
| Used by | Sweden[source] | Russian Navy and Iranian Navy[source] |
| Warhead | high explosive[source] | Conventional explosive or nuclear[source] |
8,200 mm (26 ft 11 in)[source]
Maximum; Maximum speed
Single source45 kn (83 km/h)[source]
Maximum; Maximum speed
Single sourceMaximum; Launch speed
Single sourceMaximum; Launch speed Maximum speed: in excess of
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]
Maximum; +
Single source+50 km (27 nmi)[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]
Warhead weight
Single source210 kg (460 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Engine | Pump jet[source] | Solid-fuel rocket[source] |
|---|
| Propellant | Kerosene and Hydrogen peroxide[source] | Solid-fuel[source] |
|---|
| Maximum depth | >500 m[source] | — |
|---|
| Launch platform | Gotland class Södermanland class Future A26 submarine[source] | 533 mm (21 in) torpedo tubes[source] |
|---|
| In service | — | 1977–present[source] |
|---|
| Designer | — | NII-24 research institute[source] |
|---|
| Designed | — | 1960s–70s[source] |
|---|
| Manufacturer | — | Tactical Missiles Corporation[source] |
|---|
| Produced | — | 1977–present[source] |
|---|
| Variants | — | Shkval 2, Shkval-E[source] |
|---|
| Guidance system | — | GOLIS autonomous inertial guidance[source] |
|---|
| Reported operators | — |
|
|---|
Maximum; Maximum speed or greater
Single source