| غوری-II/حتف-VA | |
|---|---|
| قسم | MRBM |
| مقام آغاز |  پاکستان |
| تاریخ ا استعمال | |
| استعمال از | پاکستان |
| تاریخ صنعت | |
| ڈیزائنر | Khan Research Laboratories (کے آر ایل) |
| صنعت کار | Khan Research Laboratories (کے آر ایل) |
| تفصیلات | |
| وزن | 17,800 کلو گرام |
| لمبائی | 18.00 میٹر |
| قطر | 1.35 میٹر |
| Warhead | 1200 کلو روایتی یا جوہری |
| انجن | Single-stage liquid propellant rocket motor |
| Propellant | Liquid fuel |
Operational range | 1500-1800 km[1][2] |
Guidance system | Inertial guidance system (INS)، GPS satellite guidance |
Launch platform | Transporter erector launcher (TEL) |
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