Pakistan Missile Technology
Ghauri I
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| Ghauri-I / Hatf-V | |
|---|---|
| External Image 1 Ghauri ballistic missile just before a test launch, Pakistan. | |
| Type | Medium-Range Ballistic Missile (MRBM) |
| Place of origin | |
| Service history | |
| In service | 12 January 2003 |
| Used by | |
| Production history | |
| Manufacturer | Kahuta Research Laboratories (KRL) |
| Specifications | |
| Weight | 15,850 kg |
| Length | 15.90 m |
| Diameter | 1.35 m |
| Engine | Single stage liquid fuel rocket motor |
| Propellant | Liquid fuell |
| Operational range | 1,500 km |
| Flight altitude | 350 km reached in first test flight |
| Guidance system | Inertial Guidance system ( INS ) |
| Launch platform | transporter erector launcher ( TEL) |
The Hatf V, named Ghauri-I (Urdu: غوری), is a medium-rang ballistic missile (MRBM) developed by Kahuta Research Laboratories (KRL) of Pakistan . Powered by a single stage liquid fuel rocket motor, the missile has an optimum range of 1,500 km and can carry a payload of 700 kg. Two variants of the Ghauri were produced under the Pakistani missile research and development program and the development of a third was cancelled.
The Ghauri II uses increased motor assembly length and improved propellants for an increased range of 2,300 km (1,400 mi).The Ghauri-V had a planned range of 4,500–6,000 km.
The missile is named after the Turkic ruler Shahabuddin Muhammad Ghauri of what today is Afghanistan , while the "Hatf" designation originates from the name of the sword or lance of the Prophet Muhammad .