 | Tsikada
| Article Number: 11F643. Class: Navigation. Destination: Medium Earth Orbit. Nation: Russia. Agency: MO SSSR. Manufacturer: Reshetnev. Tsikada was a complementary civilian version of the Parus military naval navigation satellite system for the Soviet Merchant Marine and Academy of Sciences. Development began once flight test of Parus began in 1974, and deployment of the operational Tsikada system began in 1978. Development of this second generation Soviet navigation satellite system represented a collaboration between the Navy, Academy of Sciences, and Ministry of Shipping. The basis was the Parus / Tsiklon-B Doppler navigation system, but allowing asynchronous operation of on-board equipment with only essential equipment receiving a timer interrupt.
Development began in 1974 with most preliminary work already accomplished under the military Parus program. Prime contractor was KBPM/Reshetnev. PO Polyot, A S Klinyshkov Chief Designer, provided synchronization equipment. NII Radiopribor under N Ye Ivanov provided cryptography and spacecraft navigation systems. Flight trials began in 1976 from Plesetsk under Admiral A I Rassokho. The launch of Kosmos 1000 on 31 March 1978 marked the beginning of deployment of the operational system. The system was accepted for military service in 1979 by the Soviet Army and VMF.
The operational satellite constellation consisted of a minimum of four operational satellites, each deployed in one of four planes, spaced 45 degrees apart. Typical lifetime was 18 to 24 months.
The signals were supplemented for military users by the very similar military Tsiklon-B/Parus system, which was in six planes 30 degrees apart. The satellites transmitted Doppler-shifted VHF transmissions at around 150 and 400 MHz of their position and orbital characteristics.
The satellite could be launched one per Kosmos-3M or four per Tsyklon-3 booster. The Tsikada system provided global navigation for both the Soviet Navy and commercial shipping. Typical orbit: 965 km x 1009 km at 83 degrees inclination. Mass: 820 kg (1,800 lb). Electrical System: Solar cells on exterior. Electric System: 0.20 average kW. Associated Launch Vehicle: Kosmos 11K65M. Tsikada Chronology
- 1991 February 5 - Cosmos 2123 - Launch Site: Plesetsk. Launch Vehicle: Kosmos 11K65M. Mass: 810 kg (1,780 lb). Perigee: 963 km (598 mi). Apogee: 1,005 km (624 mi). Inclination: 82.90 deg. Period: 104.80 min.
Civilian navigation satellite. Positioned in plane 13 of constellation. Testing of components and equipment of a space navigation system being set up to determine the position of civil aircraft and ships of the USSR merchant marine and fishing fleet at any point on the oceans and seas. Two amateur satellite transponders, RS12 and RS13, were secondary payloads on the Cosmos 2123 navigation satellite. These transponders were developed at the Kaluga Electromechanical Plant under the direction of Aleksander Papkov and were launched aboard several satellites by the USSR during 1978-1991.
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.
- Golotyuk, S, Novosti kosmonavtiki, "Sputnikostroiteli s beregov Yeniseya", No. 10, 1999, p. 64.
- Melnik, T G, Voenno-Kosmicheskiy Siliy, Nauka, Moscow, 1997.. Two-volume official history of the (now defunct) Russin space forces.
- Novosti Kosmonavtiki, "Rossiya. V polyote 'Kosmos-2345'", 1997, Issue 17, page 31.
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