Kh-101 / Kh-102
| Specifications | ||
|---|---|---|
| Contractor | Raduga Machine Design Bureau | |
| Designation | Kh-101 | Kh-65 / Kh-SD |
| Type | ground attack standoff cruise missile |
|
| First Flight | 1999 | |
| Length m | 7.45 | |
| Diameter, mm | 742 | |
| Wingspan, m 3 | ||
| RCS , m² | 0.01 | |
| Starting weight, kg | 2200-2400 | 1,400-1,800kg |
| Warhead Weight kg | 400 | |
| Fuel weight, kg | 1250 | |
| Speed, m / c, cruising | 190-200 | |
| Speed, m / c, maximal | 250-270 | |
| Max. speed | Mach 0.75 | Mach 0.75 |
| Height of flight, m | from 30-70 to 10 000 | |
| Ceiling | ||
| flight profile | changeable | |
| Launch range, km | 4500-5500 or 3,000-5,000 km on different data | ? 300-500 km |
| Propulsion | solid booster + cruise turbofan | |
| Engine | DTRD turbofan-50A @ 450 kgf | |
| Guidance |
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| Accuracy (CWE), m | 5-6 | |
| Warhead |
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| carriers |
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