Iskander / SS-26
| Specifications | |||||||
|---|---|---|---|---|---|---|---|
| DIA Code Name | SS-26 | ||||||
| Nato Code Name: | ? | ||||||
| Russian Designation: | Iskander | ||||||
| Design Bureau: | KBM Engineering | ||||||
| Inservice: | 1999?? / 2007 ?? | ||||||
| Range: | maximum 280 Km ? / 500 km ? minimum 50 Km | ||||||
| Stages: | 1 | ||||||
| Fuel: | Solid | ||||||
| In service: | Current System | ||||||
| Contractor | |||||||
| Entered Service | |||||||
| Total length | |||||||
| Diameter | |||||||
| Wingspan | |||||||
| launcher Weight | 40,000 kg | ||||||
| Missile Weight | 3,800 kg | ||||||
| Warhead Weight | 480 kg | ||||||
| Maximum Speed | |||||||
| Guidance mode | independent, inertial, integrated with optical homing head | ||||||
| Single-shot hit probability | |||||||
| Warhead | cluster, HE fragmentation, penetrating, HE incendiary | ||||||
| Chassis | wheeled, cross-country | ||||||
| Number of missiles: | |||||||
| on launcher | 2 | ||||||
| on transloader | 2 | ||||||
| Time to launch, min: | |||||||
| from highest readiness state | up to 4 | ||||||
| after march | up to 6 | ||||||
| Assigned service life | yr 10 | ||||||
| Crew | 3 | ||||||
| Operating temperature range | °C ±50 | ||||||
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