Angara-1.2
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Angara-1.2
"Angara-1.2" is a Russian two-stage small-lift launch vehicle designed to launch a payload of up to 3.5 tons into low Earth orbit and up to 2.4 tons into a Sun-synchronous orbit, sun—synchronous orbit. The height of the "Angara-1.2" is about 41.5 m, the launch mass of the rocket is about 171 tons. It is part of the Angara (rocket family), Angara family of launch vehicles. Description The Angara-1.2 rocket has two stages running on cryogenic fuel, the fuel is kerosene of the RG-1 naphthyl brand, and the oxidizer is liquid oxygen. Since the second stage does not have the possibility of re-activation to form the final orbit of the spacecraft being launched, it includes a detachable orbital launch unit "AM" (aggregate module) operating on high-boiling fuel dinitrogen tetroxide + UDMH "Unsymmetrical dimethylhydrazine, heptyl". First Stage The first stage of the Angara-1.2 is a Universal Rocket Module, universal rocket module, similar to those used on the first and second stages ...
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Plesetsk Cosmodrome Site 35
Site 35 at the Plesetsk Cosmodrome is a launch complex used by the Angara rocket. The complex has a single launch pad, Site 35/1, which was first used for the maiden flight of the Angara in July 2014. Zenit Site 35 was originally intended to support the Zenit rocket, which the Soviet Union saw as a replacement for the R-7 series. The construction of a Zenit launch complex at Plesetsk was authorised in 1976; however, development did not begin until the completion of Site 45 at the Baikonur Cosmodrome, which was also constructed for Zenit. Construction at Site 35 began in the mid-1980s, but the programme was abandoned following the dissolution of the Soviet Union. Following the cancellation of Zenit launches from Plesetsk, Russia had originally planned to use parts constructed for Site 35 to repair one of the Zenit pads at Baikonur that had been heavily damaged when a rocket lost thrust and fell back into the flame trench seconds after launch. Instead, the parts were eventually use ...
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