Credit
Saberwyn · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Double Eagle Mark II · Length
Single sourceDouble Eagle original · Length
Single sourceConfiguration
| Specification | Double Eagle (mine disposal vehicle) | MAGURA V5 |
|---|---|---|
| Complement | — | Not applicable |
| Type | remotely operated vehicle (ROV)[source] | Unmanned surface vehicle[source] |
| Manufacturer | Saab Underwater Systems AB[source] | — |
| Role | disposal of naval mines[source] | — |
| Depth | 500 metres (1,600 ft)[source] 500 metres (1,600 ft)[source] |
Length
Single source5.5 m (18 ft)[source]
Operational; up to
Single sourceup to 800 km (500 mi)[source]
Double Eagle Mark II · brushless electric motors for fine manoeuvering
Single sourceDouble Eagle Mark III · four brushless electric motors as main thrusters
Single sourceDouble Eagle Mark II · two brushless electric motors for main propulsion, and six
Single sourcetwo 5 kilowatt brushless electric motors for main propulsion, and six 0.4 kilowatt brushless electric motors for fine manoeuvering[source]
four 7 kilowatt brushless electric motors as main thrusters[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Sensors | scanning sonar, echo locations , doppler logs , or self-navigation systems[source] | — |
|---|
| Relative dimensions | The Mark III is 80 centimetres (31 in) longer and 130 kilograms (290 lb) heavier than its predecessor.[source] | — |
|---|
| Country of origin | Sweden[source]Inventory Origin column; table 3, row 44, cell 4; revision 1374738459; retrieved 2026-09-30 | — |
|---|
| Place of origin | — | Ukraine[source] |
|---|
| Used by | — | Main Directorate of Intelligence in conjunction with the 385th USV Brigade[source] |
|---|
| Unit cost | — | $273,000[source] |
|---|
| Variants | — | See variants[source] |
|---|
| Main armament | — | Explosive charge up to 300 kg (660 lb) or Sea Dragon surface-to-air missile (modified R-73 air-to-air missile)[source] |
|---|
| Guidance system | — | GNSS , inertial , visual[source] |
|---|