The Zenit-3SL design began in the late 1980s as the Zenit-3, a proposed replacement for the
Proton-K, which would have used a
Zenit-2 rocket with a
Block D upper stage. This proposal was shelved after the
dissolution of the
Soviet Union, as Russia inherited the space programme, however the Zenit was manufactured in
Ukrainian SSR. Boeing became involved in the programme in 1994. The design was subsequently modified, with a modified version of the
Block DM replacing the Block D. Sea Launch integrated the rockets in
California, and transferred them to Odyssey via the
Sea Launch Commander for transportation to the launch site. Once at the launch site, the rocket was erected on the platform, and a three-day countdown was initiated. The countdown was fully automated, and personnel were evacuated from the launch platform to
Commander prior to launch. Zenit-3SL launches predominantly carried
communications satellites into
geosynchronous transfer orbits. As of 2009, the only payload to be launched by a Zenit-3SL that was not a communications satellite was a
DemoSat, on the maiden flight. The only launch to be conducted to an orbit other than GTO was that of
ICO F-1, which was intended to be placed into
medium Earth orbit, however the rocket failed to reach orbit. ==Reliability==