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Other Designations: I1P. Manufacturer's Designation: I1. Class: Military. Type: ASAT. Nation: Russia. Agency: NII-88. Manufacturer: Chelomei. 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 maneuvering 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. Typical orbit: 300 km x 1420 km at 59 degrees inclination. Mass: 1,400 kg (3,000 lb). Associated Launch Vehicle: Polyot 11A59. Polyot Chronology
Bibliography and Further Reading
- McDowell, Jonathan, Jonathan's Space Home Page, Harvard University, 1997-present. Jonathan McDowell's complete on-line listing of all objects orbited and over 20,000 rocket launches Accessed at: http://www.planet4589.org/jsr.html.
- Tarasenko, M, Novosti kosmonavtiki, "30 let sevodnya - pervovo sputnikovo perkhvali", No. 23/24, 1998, p. 40..
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