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Polyot 1 - Credit: © Mark Wade. 16,155 bytes. 221 x 402 pixels. |
First prototype model of Chelomei's ASAT, used in an interceptor control and propulsion test. Launched by Korolev R-7 because Chelomei's own UR-200 was not yet available. Purpose - elaboration of system providing for the extensive manoeuvring of space apparatuses. Flight was considered a great success. Micro-engine fired 350 times and main stabilizing engine fired 300 times. Polyot was equipped with 6 x 400 kgf engines and 16 x 1 kgf verniers. It consisted of a cylindrical guidance section, the engine section with spherical propellant tanks, and the forward warhead section.
Total Mass: 1,400 kg.
ASAT interceptor control and propulsion test. Launched by Korolev R-7 because Chelomei's own UR-200 was not yet available. Purpose - elaboration of system providing for the extensive manoeuvring of space apparatuses. Flight was considered a great success. Micro-engine fired 350 times and main stabilizing engine fired 300 times. Orbit given is final orbit after manoeuvres.