Model: Ghauri. Intermediate range ballistic missile. Family: Scud. Other Family: Active. Country: Pakistan. Status: Active. Other Designations: Hatf 5.
Derivative of North Korean No Dong. First fired April, 1998. Payload is about 700 kg. Managed by A Q Khan Research Laboratories.
Manufacturer: Pakistan. Launches: 7. Success Rate: 100.00%. First Launch Date: 1998-04-06. Last Launch Date: 2006-11-16. Launch data is: continuing. Apogee: 150 km (90 mi). Liftoff Thrust: 255.000 kN (57,326 lbf). Total Mass: 14,500 kg (31,900 lb). Core Diameter: 1.19 m (3.90 ft). Total Length: 14.82 m (48.61 ft). Standard warhead mass: 700 kg (1,540 lb). Maximum range: 1,200 km (700 mi). Boost Propulsion: Storable liquid rocket. Guidance: Inertial.
- Stage1: 1 x Ghauri. Gross Mass: 16,000 kg (35,000 lb). Empty Mass: 3,000 kg (6,600 lb). Motor: 1 x Nodong. Thrust (vac): 255.000 kN (57,326 lbf). Burn time: 110 sec. Length: 16.00 m (52.00 ft). Diameter: 1.30 m (4.20 ft). Propellants: Nitric acid/UDMH.
Ghauri Chronology
1998 April 6 - Tilla -. Test mission Agency: Pakistan. Apogee: 150 km (90 mi).
1999 April 14 - 05:35 GMT - Tilla -. Ghauri Ghauri-2/Hatf-6 Test mission Agency: Pakistan. Apogee: 150 km (90 mi).
2002 May 25 - 04:30 GMT - Tilla -. Ghauri Ghauri II Test mission Agency: Pakistan. Apogee: 150 km (90 mi).
2004 May 29 - Tilla -. Ghauri test Agency: Pakistan. Apogee: 150 km (90 mi).
2004 June 4 - Tilla -. Test mission Agency: Pakistan. Apogee: 150 km (90 mi).
2004 October 12 - Tilla -. Ghauri test Agency: Pakistan. Apogee: 150 km (90 mi).
2006 November 16 - Tilla -. Ghauri Haft-5 Ghauri test launch Agency: Pakistan. Apogee: 100 km (60 mi).
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