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8K14
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Family: Miscellany. Country: Iraq. Status: Hardware.
Iraqi space launch vehicle/ICBM based on clustering of Scud tactical missiles. Canadian rocket scientist Gerald Bull was allegedly killed by Israeli agents not for his work on the supergun, but rather for his much more damaging assistance to the Iraqis in doing the dynamic calculations for the Tamouz.
SpecificationsLaunches: 1. Failures: 0. Success Rate: 100.00% pct. First Launch Date: 05 December 1989. Last Launch Date: 05 December 1989. Liftoff Thrust: 41,440 kgf. Total Mass: 37,695 kg. Core Diameter: 1.0 m. Total Length: 18.0 m.
- Stage Number: 0. 5 x R-17 Gross Mass: 5,385 kg. Empty Mass: 1,645 kg. Thrust (vac): 9,500 kgf. Isp: 251 sec. Burn time: 95 sec. Isp(sl): 219 sec. Diameter: 1.0 m. Span: 1.8 m. Length: 7.4 m. Propellants: Nitric acid/Kerosene No Engines: 1. Isayev R-17
- Stage Number: 1. 1 x R-17 Gross Mass: 5,385 kg. Empty Mass: 1,645 kg. Thrust (vac): 9,500 kgf. Isp: 251 sec. Burn time: 95 sec. Isp(sl): 219 sec. Diameter: 1.0 m. Span: 1.8 m. Length: 7.4 m. Propellants: Nitric acid/Kerosene No Engines: 1. Isayev R-17
- Stage Number: 2. 1 x R-17 Gross Mass: 5,385 kg. Empty Mass: 1,645 kg. Thrust (vac): 9,500 kgf. Isp: 251 sec. Burn time: 95 sec. Isp(sl): 219 sec. Diameter: 1.0 m. Span: 1.8 m. Length: 7.4 m. Propellants: Nitric acid/Kerosene No Engines: 1. Isayev R-17
Tamouz Chronology
1989 Dec 5 - LV Configuration: Tamouz-1 (1 stage). Launch Site: Al Anbar .
- Research and Development Flight
Suborbital.
1990 Mar 22 -
Bibliography:- 45 - Koelle, Heinz Hermann,, Handbook of Astronautical Engineering, McGraw-Hill,New York, 1961.
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Last update 12 March 2001.
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© Mark Wade, 2001 .