| 词条 | R-26 (missile) |
| 释义 |
| name = R-26 | image = | caption = | origin = {{flagcountry|USSR}} | type = Intercontinental ballistic missile | is_missile = yes | service = | used_by = | designer = | design_date = 1960-1961 | manufacturer = | unit_cost = | production_date = | number = | variants = | spec_label = | weight = {{convert|87000|kg|lb|abbr=on}}[1] | length = | part_length = | width = | height = | diameter = | filling = | filling_weight = | detonation = | yield = | engine = | engine_power = | pw_ratio = | fuel_capacity = | vehicle_range = {{convert|12000|km|nmi}}[1] | speed = | guidance = | steering = | propellant = Liquid fuel | ceiling = | altitude = | boost = | accuracy = CEP {{convert|2000|m|ft}}[1] | launch_platform = | transport = }} The R-26 was a second-generation intercontinental ballistic missile (ICBM) designed but not deployed by the Soviet Union during the Cold War. Control system of it was designed at NPO "Electropribor"[2] (Kharkiv, Ukraine). The missile was mistakenly identified as an R-9 Desna and given the NATO reporting name SS-8 Sasin. Within the Soviet Union, it carried the GRAU index 8K66. DevelopmentDesign of the R-26 was initiated to develop a light liquid propellant powered ICBM. Designs received approval in 1960, but prior to flight tests were cancelled by the government in 1962. The missile was revealed during a Red Square parade in November 1964, where it was misidentified as an R-9 Desna. However, the program had already been cancelled and the error was not rectified. Operators
See also
External links
References1. ^1 2 http://www.globalsecurity.org/wmd/world/russia/r-26-specs.htm {{Russian and Soviet military designation sequences}}{{Russian and Soviet missiles}}{{Missile-stub}}2. ^Krivonosov, Khartron: Computers for rocket guidance systems 2 : Cold War intercontinental ballistic missiles of the Soviet Union|Intercontinental ballistic missiles of the Soviet Union |
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