FROG-7A (3R-11, 9K21, 9M21, R-65)
FROG-7B (9K52, 9M52, R-70), Luna-M
| Specifications | ||
|---|---|---|
| Contractor | Barricades factory | |
| Entered Service | 1964 | |
| Users | CIS, Cuba, Egypt, Iraq, Kuwait, Libya, North Korea, Syria, Yemen | |
| MISSILE | 9M21 | |
| Total length | 8960 - 9400 mm (7A) 9.2 meters / 30 feet (7B) 9.6 meters / 31.3 feet | |
| Diameter | 1.8 feet / 540 mm | |
| Wingspan | ||
| Weight | 2.5-2.8 tons / 2432-2486 kg | |
| Warhead Weight | 200-450kg / 550 kg | |
| Propulsion | solid | |
| Maximum Speed | 1200 m/s | |
| Maximum effective range | 68-70 km | |
| Firing range, minimum | 12-15 | |
| Guidance mode | ballistic | |
| Accuracy (dispersion) | 500-700 m [Russian estimate] impact area 2.8 km long by 1.8 km wide [Western estimate] | |
| MISSILE | 9P113 | |
| Base | ZIL-135LM (8x8) | |
| mass of PU with a rocket, kg | 17560 | |
| Number of guides, pcs | one | |
| Guide length mm | 9970 | |
| Guide elevation angle, degrees: - maximum | 65 | |
| Guide elevation angle, degrees: - minimum | 15 | |
| Horizontal guidance angle, degrees | ± 7 | |
| Maximum speed, km / h | 60 | |
| Cruising range, km | 850 | |
| Crane lifting capacity, kg | 3000 | |
| BM preparation time for shooting, min | 15-30 | |
| Crew, people | 7 | |
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