Kurchev-2: Difference between revisions
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The '''Kurchev-2''' was developed to be the successor to the [[Kurchev-1]], designed to have a longer range but |
The '''Kurchev-2''' was developed to be the successor to the [[Kurchev-1]], designed to have a longer range but failed to reach the expectations set by the Iphelklorian government. |
Latest revision as of 22:20, 21 February 2021
This page (or section) is a work in progress by its author(s) and should not be considered final. |
Kurchev-2 | |
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Type | Medium-range ballistic missile (MRBM) |
Place of origin | Iphelklori |
Service history | |
In service | 1956-1963 |
Used by | Iphelklori |
Wars | 1960 Victograd Border Conflict |
Production history | |
Designer | Arms Research and Development Division |
Designed | 1954-1955 |
Manufacturer | Gustavski corporation |
Produced | 1956–1961 |
Number built | 140 |
Variants | Juno II |
Specifications | |
Weight | 49,800 kg (110,000 lb) |
Length | 18.3 m (60 ft) |
Diameter | 2.67 m (8 ft 9 in) |
Warhead | W38 Warhead 3.75 Mt or W49 1.44 Mt |
Blast yield | 3.75 Mt or 1.44 Mt |
Engine | Gustavski RE-NA (Model S-3D) liquid LRE 150,000 lbf (667 kN) |
Propellant | kerosene and liquid oxygen |
Operational range | 1,500 mi (2,400 km) |
Flight ceiling | 610 km (380 mi) |
The Kurchev-2 was developed to be the successor to the Kurchev-1, designed to have a longer range but failed to reach the expectations set by the Iphelklorian government.