K-60 HVDV: Difference between revisions
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{{Infobox weapon | {{Infobox weapon | ||
| name = | | name = K-60 High Velocity Delivery Vehicle | ||
| image = | | image = File:HypersonicMissileBomber.png | ||
| image_size = | | image_size = 400 | ||
| alt = | | alt = | ||
| caption = | | caption = Diagram constructed from external views of the Vessel. | ||
| type = {{wp|Intercontinental Ballistic | | type = {{wp|Intercontinental Ballistic High Velocity Aircraft}} | ||
| origin = [[ | | origin = [[Kalaron]] | ||
<!-- Type selection --> | <!-- Type selection -->S | ||
| is_ranged = | | is_ranged = | ||
| is_bladed = | | is_bladed = | ||
| Line 16: | Line 16: | ||
| is_UK = | | is_UK = | ||
<!-- Service history --> | <!-- Service history --> | ||
| service = | | service = 2015 — Present | ||
| used_by = [[Californian Empire]] | | used_by = [[Californian Empire]] | ||
| wars = | | wars = | ||
<!-- Production history --> | <!-- Production history --> | ||
| designer = | | designer = Kalaron Arms | ||
| design_date = 12 October | | design_date = 12 October 2012 | ||
| manufacturer = | | manufacturer = Kalaron Arms | ||
| unit_cost = | | unit_cost = Payload Dependent | ||
| production_date = 29 August | | production_date = 29 August 2015-Present | ||
| number = | | number = 75 | ||
| variants = | | variants = | ||
<!-- General specifications --> | <!-- General specifications --> | ||
Latest revision as of 02:27, 12 March 2021
| K-60 High Velocity Delivery Vehicle | |
|---|---|
 Diagram constructed from external views of the Vessel. | |
| Type | Intercontinental Ballistic High Velocity Aircraft |
| Place of origin | Kalaron S |
| Service history | |
| In service | 2015 — Present |
| Used by | Californian Empire |
| Production history | |
| Designer | Kalaron Arms |
| Designed | 12 October 2012 |
| Manufacturer | Kalaron Arms |
| Unit cost | Payload Dependent |
| Produced | 29 August 2015-Present |
| No. built | 75 |
| Specifications (Specifications) | |
| Weight | 215,600 kg (475,300 lb) |
| Length | 36.9 m (121 ft) |
| Diameter | 3.05 m (10.0 ft) |
| Warhead | 20 × 750 kiloton warheads, 1 × 5 megaton warhead |
Detonation mechanism | Airburst |
| Engine | Three Stage Liquid Propellant |
Operational range | 10,200 km (6,300 mi)—16,000 km (9,900 mi) |
| Speed | Up to 8.4 km/s |
Guidance system | Inertial, Autonomous |
| Accuracy | 110-350 m CEP (depending on missile variants) |
Launch platform | Silo, TEL |
| Transport | TEL |
| References | |