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Tamouz

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Tamouz

AKA: Abid. Status: Retired 1989. First Launch: 1989-12-05. Last Launch: 1989-12-05. Number: 1 . Thrust: 406.40 kN (91,362 lbf). Gross mass: 37,695 kg (83,103 lb). Height: 18.00 m (59.00 ft). Diameter: 0.96 m (3.14 ft). Apogee: 100 km (60 mi).

Maximum range: 2,000 km (1,200 mi).

Stage Data - Tamouz

• Stage 0. 5 x R-17. Gross Mass: 5,385 kg (11,871 lb). Empty Mass: 1,645 kg (3,626 lb). Thrust (vac): 93.100 kN (20,930 lbf). Isp: 251 sec. Burn time: 95 sec. Isp(sl): 219 sec. Diameter: 0.96 m (3.14 ft). Span: 1.77 m (5.80 ft). Length: 7.43 m (24.37 ft). Propellants: Nitric acid/Kerosene. No Engines: 1. Engine: Isayev R-17. Other designations: 8K14, SS-1C Scud B, 9K72 Elbrus. Status: Out of Production. Comments: Developed from Russian storable fuel tactical missile. Original R-11 designed by Korolev OKB, subsequent developments by Makeyev OKB. Using calculations of Gerald Bull, stretched and clustered as basis of Iraqi ICBM/satellite launch vehicle.

• Stage 1. 1 x R-17. Gross Mass: 5,385 kg (11,871 lb). Empty Mass: 1,645 kg (3,626 lb). Thrust (vac): 93.100 kN (20,930 lbf). Isp: 251 sec. Burn time: 95 sec. Isp(sl): 219 sec. Diameter: 0.96 m (3.14 ft). Span: 1.77 m (5.80 ft). Length: 7.43 m (24.37 ft). Propellants: Nitric acid/Kerosene. No Engines: 1. Engine: Isayev R-17. Other designations: 8K14, SS-1C Scud B, 9K72 Elbrus. Status: Out of Production. Comments: Developed from Russian storable fuel tactical missile. Original R-11 designed by Korolev OKB, subsequent developments by Makeyev OKB. Using calculations of Gerald Bull, stretched and clustered as basis of Iraqi ICBM/satellite launch vehicle.

• Stage 2. 1 x R-17. Gross Mass: 5,385 kg (11,871 lb). Empty Mass: 1,645 kg (3,626 lb). Thrust (vac): 93.100 kN (20,930 lbf). Isp: 251 sec. Burn time: 95 sec. Isp(sl): 219 sec. Diameter: 0.96 m (3.14 ft). Span: 1.77 m (5.80 ft). Length: 7.43 m (24.37 ft). Propellants: Nitric acid/Kerosene. No Engines: 1. Engine: Isayev R-17. Other designations: 8K14, SS-1C Scud B, 9K72 Elbrus. Status: Out of Production. Comments: Developed from Russian storable fuel tactical missile. Original R-11 designed by Korolev OKB, subsequent developments by Makeyev OKB. Using calculations of Gerald Bull, stretched and clustered as basis of Iraqi ICBM/satellite launch vehicle.