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T-5E 'Luna-M' Rocket Launcher |
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T-5E 'Luna-M' (FROG-7) |
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Manufacturer: |
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Role: |
Battlefield Support Missile |
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Russian Designation: Military Designation: Military Industrial Number: |
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Year Adopted: |
1965 (FROG-7a) |
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Number Produced: | 2000 (approximately) | ||||||
Weight: | 23 Tons | ||||||
Operational Status: |
CIS, Cuba, Egypt, Iraq, Kuwait, Libya, North Korea, Syria, Yemen and some Warsaw Pact nations. |
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Armament: |
1 x R-65, R-70, or R-75 Rocket with either a conventional or nuclear warhead. |
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Engine: |
2x V-8 water-cooled gasoline engines producing a total of 180 horsepower @ 3200 RPM |
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Crew: |
4 men |
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Base Vehicle: | Zil-135 (8x8) | ||||||
Armor: | None | ||||||
Length: |
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Height: |
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Width: |
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Maximum Speed: |
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Range of Vehicle: |
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T-5E 'Luna-M' Rocket Statistics |
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Rocket Variant: | R-65 | R-70 | R-75 | ||||||
Article Number: | 9K21 | 9K52 | 9K52 | ||||||
NATO Designation: | FROG-7a | FROG-7a | FROG-7b | ||||||
Maximum Range: |
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Minimum Range: | 11km (6.8
miles) High Explosive or Nuclear (10, 100, or 200kt) |
14km (8.7 miles) Chemical |
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Warheads: |
550kg (1213 lb) High Explosive or Nuclear (10, 100, or 200kt) |
390kg (860 lb) Chemical |
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Fuel: | Solid Fuel | Solid Fuel | Solid Fuel | ||||||
Circular Error of Probability (CEP): |
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Length: |
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Uncertain | ||||||
Diameter: |
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Uncertain | ||||||
Wingspan: |
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Uncertain | ||||||
Rocket Weight: |
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Uncertain |