Status: Cancelled 1957.
Design work starts on the Zenit, the first military photo-reconnaisance satellite. The necessary subsystems were defined incrementally throughout 1956 in a series of specification documents. In April the specifications for a redundant restartable engine and appropriate satellite guidance and control systems were released. In May the technical requirements document was issued for a satellite that could be oriented in orbit. In July tests began of appropriate heat shield materials.
The decree formally authorised design of a military reconnaissance satellite. In October the specification was issued for a comprehensive research program leading to manoeuvrable spacecraft. By April 1957 the military issued a requirements document for experimental solar cell panels. Design bureau work on the reconnaissance satellite began in 1957 in Section 3 of OKB-1 (Tikhonravov and Ryazanov). This spacecraft was initially sized at 1.5 tonnes total for launch by the basic R-7 rocket.
These included development of a three stage version of R-7, development of satellite guidance and control systems of the precision required for photography from orbit, satellite control equipment, ELINT sensors, guidance systems, film cassette return systems, and tracking systems for recovery of the re-entry vehicle with the film cassette.