Kurchev-13: Difference between revisions
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BeeKayGodd (talk | contribs) (Created page with "Category:Art's Links {{WIP}}{{Infobox weapon |is_missile=yes |name=Kurchev-13 |origin=Iphelklori |image=Dong-Feng_26.JPG |caption=A Kurchev-13 during the 2018 Armed Fo...") |
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|wingspan= |
|wingspan= |
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|speed= |
|speed= |
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|vehicle_range=2, |
|vehicle_range=2,700–7,000 km (est.) |
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|ceiling= |
|ceiling= |
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|altitude=2,111.5 km at lofted trajectory (which reduces range to 787 km) |
|altitude=2,111.5 km at lofted trajectory (which reduces range to 787 km) |
Latest revision as of 06:07, 23 January 2021
This page (or section) is a work in progress by its author(s) and should not be considered final. |
Kurchev-13 | |
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Type | Ballistic missile, Mobile IRBM/ICBM |
Place of origin | Iphelklori |
Service history | |
In service | 2014-Present |
Used by | Iphelklori |
Production history | |
Manufacturer | Gustavoski Corporation |
Produced | 2014-2017 |
Specifications | |
Weight | 24.7 tons (est.) |
Height | 16.5 m (est.) |
Diameter | 1.5 m (est) |
Warhead | Conventional |
Warhead weight | 500-650 kg (est.) |
Engine | Liquid-propellant rocket, single chamber variant of Gustavski RE-34 464.1 kN total |
Propellant | Hypergolic combination of unsymmetrical dimethylhydrazine (UDMH) as fuel, and either Dinitrogen tetroxide (Template:Chem) |
Operational range | 2,700–7,000 km (est.) |
Flight altitude | 2,111.5 km at lofted trajectory (which reduces range to 787 km) |
Guidance system | Gustaviski G-60 Mk.2 inertial guidance |
Accuracy | greater than 5 km CEP |
Launch platform | MAZ-based vehicle |