Polyot
Polet 1
Credit - © Dietrich Haeseler
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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
  • 1963 November 1 - Polet 1; Polyot 1 - Launch Site: Baikonur. Launch Vehicle: Polyot 11A59. Mass: 1,400 kg (3,000 lb). Perigee: 331 km (205 mi). Apogee: 1,420 km (880 mi). Inclination: 58.90 deg. Period: 102.40 min.

    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.

  • 1964 April 12 - Polet 2; Polyot 2 - Launch Site: Baikonur. Launch Vehicle: Polyot 11A59. Mass: 1,400 kg (3,000 lb). Perigee: 303 km (188 mi). Apogee: 479 km (297 mi). Inclination: 58.10 deg. Period: 92.30 min.

    ASAT interceptor control and propulsion test. Elaboration of systems providing for the extensive manouevring of space apparatuses.


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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