N-6
N-4 Spacecraft
Credit - Chelomei School, Leninsk
Class: Astronomy. Type: Cosmic Ray. Destination: Space Station Orbit. Nation: Russia. Agency: MOM. Manufacturer: Chelomei.

Cosmic ray measurements. Study of the nature of high and ultra-high energy cosmic rays and their interaction with atomic nuclei. Mass announced at time of launch 17,000 kg. Scientific payload 12,500 kg; operated for 100 days in orbit.

Typical orbit: 248 km x 477 km at 52 degrees inclination. Span: 4.10 m (13.40 ft). Mass: 16,000 kg (35,000 lb). Payload: 12,500 kg (27,500 lb). Associated Launch Vehicle: Proton 8K82K.


N-6 Chronology
  • 1968 November 16 - Proton 4 - Program: Proton. Launch Site: Baikonur. Launch Vehicle: Proton 8K82K. Mass: 16,000 kg (35,000 lb). Perigee: 248 km (154 mi). Apogee: 477 km (296 mi). Inclination: 51.60 deg. Period: 91.80 min.

    First launch of the Proton three-stage variant. The satellite studied the nature of high and ultra-high energy cosmic rays and their interaction with atomic nuclei. Scientific payload 12,500 kg; operated for 100 days in orbit.


Bibliography and Further Reading
  • Vladimirov, A, Novosti kosmonavtiki, "Tablitsa zapuskov RN 'Proton' i 'Proton K'", 1998, Issue 10, page 25.
  • Afanasyev, Igor, Novosti kosmonavtiki, "35 let RN Proton", 1998, Issue 5, page 40.
  • Kaesmann, Ferdinand, et. al., Journal of the British Interplanetary Society, "Proton - Development of A Russian Launch Vehicle", 1998, Volume 51, page 3.
  • 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.
 
 
 
 
 
 
 
 
 

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