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Tsiklon satellite

Spacecraft · Russia

Original archive entry. The text, images and links below are kept as they were written.

Parus
Parus
Tsiklon, its successor, Parus, and Sfera all used the KAUR-1 bus and were similar in appearance.

Russian navigation satellite.

The requirement for Tsiklon, the first prototype Soviet navigation satellite system, was identified in the late 1950's in order to provide Soviet ballistic missile submarines with accurate position fixes so that acceptable submarine-launched ballistic missile accuracy could be achieved. The draft project was approved in 1962, but development was prolonged due to very poor accuracy due to software problems and lack of accurate geodetic data. The system was finally accepted for service as an interim measure in 1972 pending deployment of the improved Tsiklon-B/Parus system.

Tsiklon was designed by Reshetnev; the navigation and control system was by NII Radiopribor (Ivanov, Chief Designer, L I Gusev, Director); with communications systems by MNIIRS MPSS (Nesvist). The Kosmos-3M launch vehicle was used.

The TTZ specification was completed by the TsYKOS MO (Space Forces) and the VMF (Soviet Navy). In 1962 research institute NII-695 completed the draft project for a Tsiklon experimental satellite. It was to use the Doppler navigation method and be placed in 800 to 1000 km altitude orbits. Development of the satellite was given to Reshetnev and experimental flights began in 1967 in order to develop a system meeting the required tactical and operational characteristics.

The shipboard installation consisted of the Tsunami system, composed of the Sirius radio station, the Signal antenna stabilization platform, the Konus-4 omnidirectional antenna, and the Kvant-L antenna. First trial were conducted with a Project 680 vessel of the Black Sea fleet and showed a position error of 3 km, which was intolerable. A large part of the problem was with inaccuracies in the software models available for predicting the spacecraft ephemerides. Work by the KIK Center resulted in a 10 to 30 times improvement in this accuracy, incorporating new information on the gravitational anomalies and geoid of the earth. Use of the revised software in 1969 showed an average error of 100 m over a five day period. Further improvement required a better mapping of the earth's gravitational anomalies. Testing of Tsiklon would continue through 1972 before an adequate operational system could be designed and the system was accepted for military service. The Parus/Tsiklon-B production system began flight tests in 1974.

Tsiklon used the basic KAUR-1 bus, consisting of a 2.035 m diameter cylindrical spacecraft body, with solar cells and radiators of the thermostatic temperature regulating system mounted on the exterior. Orientation was by a single-axis magneto-gravitational (gravity gradient boom) passive system. The hermetically sealed compartment had the equipment mounted in cruciform bays, with the chemical batteries protecting the radio and guidance equipment mounted at the center).

Electric System: 0.20 average kW.

More at: ZALIV.

Country
Russia
Launch Vehicles
R-14, Kosmos 3, Kosmos 11K65M
Bibliography
102, 107, 2, 445, 449, 6, 13315

Chronology

32 events

1962 During the Year

  • Draft project for Tsiklon experimental navigation satellite completed - . Nation: Russia. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite.

    Research institute NII-695 completed the draft project for a Tsiklon experimental navigation satellite. It was to use the Doppler navigation method and be placed in 800 to 1000 km altitude orbits. Experimental flights began in 1967 in order to develop a system meeting the required tactical and operational characteristics.

1967 May 15

11:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. Launch Pad: LC132/2. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 158 - . Payload: Tsiklon Mass Model. Mass: 750 kg (1,650 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 2801 . COSPAR: 1967-045A. Apogee: 812 km (504 mi). Perigee: 731 km (454 mi). Inclination: 74.00 deg. Period: 100.30 min. Military navigation satellite..

1967 September 27

Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: R-14. Launch Vehicle: Kosmos 11K65M. FAILURE: Launch vehicle exploded on pad.. Failed Stage: 1.
  • Tsiklon GVM - . Payload: Tsiklon Mass Model. Mass: 800 kg (1,760 lb). Nation: Russia. Agency: RVSN. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. Mass model of military navigation satellite used for booster test..

1967 November 23

15:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. Launch Pad: LC132/2. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 192 - . Mass: 775 kg (1,708 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 3047 . COSPAR: 1967-116A. Apogee: 725 km (450 mi). Perigee: 716 km (444 mi). Inclination: 74.00 deg. Period: 99.20 min. Military navigation satellite..

1968 May 7

13:58 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. Launch Pad: LC132/2. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 220 - . Mass: 775 kg (1,708 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 3229 . COSPAR: 1968-040A. Apogee: 700 km (430 mi). Perigee: 637 km (395 mi). Inclination: 74.00 deg. Period: 98.10 min. Military navigation satellite..

1969 August 13

22:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. Launch Pad: LC132/2. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 292 - . Mass: 775 kg (1,708 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 4070 . COSPAR: 1969-070A. Apogee: 733 km (455 mi). Perigee: 719 km (446 mi). Inclination: 74.10 deg. Period: 99.30 min. Military navigation satellite..

1969 October 21

12:49 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. Launch Pad: LC132/pad?. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 304 - . Mass: 795 kg (1,752 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 4138 . COSPAR: 1969-091A. Apogee: 748 km (464 mi). Perigee: 731 km (454 mi). Inclination: 74.00 deg. Period: 99.60 min. Military navigation satellite..

1970 April 11

17:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. Launch Pad: LC132/2. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 332 - . Mass: 775 kg (1,708 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 4369 . COSPAR: 1970-028A. Apogee: 736 km (457 mi). Perigee: 727 km (451 mi). Inclination: 74.00 deg. Period: 99.40 min. Military navigation satellite..

1970 August 20

14:30 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. Launch Pad: LC132/pad?. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 358 - . Mass: 875 kg (1,929 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. Decay Date: 1990-06-26 . USAF Sat Cat: 4497 . COSPAR: 1970-064A. Apogee: 342 km (212 mi). Perigee: 334 km (207 mi). Inclination: 74.00 deg. Period: 91.30 min. Identification uncertain. Possibly a Tsiklon military navigation satellite placed in incorrect orbit..

1970 October 12

13:57 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. Launch Pad: LC132/pad?. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 371 - . Mass: 775 kg (1,708 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 4578 . COSPAR: 1970-083A. Apogee: 728 km (452 mi). Perigee: 722 km (448 mi). Inclination: 74.00 deg. Period: 99.30 min. Military navigation satellite..

1970 December 12

13:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 385 - . Mass: 680 kg (1,490 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 4799 . COSPAR: 1970-108A. Apogee: 980 km (600 mi). Perigee: 973 km (604 mi). Inclination: 74.00 deg. Period: 104.60 min. Military navigation satellite..

1971 May 22

00:51 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 422 - . Mass: 680 kg (1,490 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 5238 . COSPAR: 1971-046A. Apogee: 1,005 km (624 mi). Perigee: 982 km (610 mi). Inclination: 74.00 deg. Period: 105.00 min. Military navigation satellite..

1971 December 15

04:31 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 465 - . Mass: 680 kg (1,490 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 5683 . COSPAR: 1971-111A. Apogee: 1,006 km (625 mi). Perigee: 965 km (599 mi). Inclination: 74.00 deg. Period: 104.80 min. Military navigation satellite..

1972 February 25

07:52 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 475 - . Mass: 680 kg (1,490 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 5846 . COSPAR: 1972-009A. Apogee: 996 km (618 mi). Perigee: 962 km (597 mi). Inclination: 74.00 deg. Period: 104.70 min. Military navigation satellite..

1972 May 6

11:24 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. Launch Pad: LC132/pad?. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 489 - . Mass: 680 kg (1,490 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 6019 . COSPAR: 1972-035A. Apogee: 998 km (620 mi). Perigee: 961 km (597 mi). Inclination: 74.00 deg. Period: 104.70 min. Military navigation satellite..

1972 August 16

13:40 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 514 - . Payload: Tsiklon Mass Model. Mass: 680 kg (1,490 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 6148 . COSPAR: 1972-062A. Apogee: 967 km (600 mi). Perigee: 952 km (591 mi). Inclination: 83.00 deg. Period: 104.30 min. Military navigation satellite..

1973 January 26

11:44 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC107/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 546 - . Payload: Tsiklon Mass Model. Mass: 750 kg (1,650 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 6350 . COSPAR: 1973-005A. Apogee: 564 km (350 mi). Perigee: 537 km (333 mi). Inclination: 50.70 deg. Period: 95.70 min. Military navigation satellite..

1973 May 25

Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M. FAILURE: Launch vehicle failed to orbit - unknown cause.. Failed Stage: U.

1973 June 20

06:16 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 574 - . Mass: 550 kg (1,210 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 6707 . COSPAR: 1973-042A. Apogee: 1,010 km (620 mi). Perigee: 976 km (606 mi). Inclination: 83.00 deg. Period: 105.00 min. Military navigation satellite..

1973 September 14

00:31 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 586 - . Mass: 550 kg (1,210 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 6828 . COSPAR: 1973-065A. Apogee: 1,003 km (623 mi). Perigee: 961 km (597 mi). Inclination: 82.90 deg. Period: 104.70 min. Military navigation satellite..

1973 December 29

04:12 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 627 - . Mass: 550 kg (1,210 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 7008 . COSPAR: 1973-109A. Apogee: 1,014 km (630 mi). Perigee: 967 km (600 mi). Inclination: 83.00 deg. Period: 104.90 min. Military navigation satellite..

1974 January 17

10:07 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 628 - . Mass: 550 kg (1,210 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 7094 . COSPAR: 1974-001A. Apogee: 1,008 km (626 mi). Perigee: 952 km (591 mi). Inclination: 83.00 deg. Period: 104.70 min. Military navigation satellite..

1974 June 27

15:40 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 663 - . Mass: 680 kg (1,490 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 7349 . COSPAR: 1974-048A. Apogee: 999 km (620 mi). Perigee: 963 km (598 mi). Inclination: 83.00 deg. Period: 104.70 min. Military navigation satellite..

1974 October 18

22:36 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 689 - . Mass: 680 kg (1,490 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 7476 . COSPAR: 1974-079A. Apogee: 1,015 km (630 mi). Perigee: 972 km (603 mi). Inclination: 82.90 deg. Period: 105.00 min. Military navigation satellite..

1975 April 22

21:10 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 729 - . Mass: 725 kg (1,598 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 7768 . COSPAR: 1975-034A. Apogee: 1,007 km (625 mi). Perigee: 971 km (603 mi). Inclination: 83.00 deg. Period: 104.90 min. Military navigation satellite..

1976 February 3

08:16 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 800 - . Mass: 650 kg (1,430 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 8645 . COSPAR: 1976-011A. Apogee: 1,009 km (626 mi). Perigee: 978 km (607 mi). Inclination: 83.00 deg. Period: 105.00 min. Military navigation satellite..

1976 June 2

22:30 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 823 - . Mass: 650 kg (1,430 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 8873 . COSPAR: 1976-051A. Apogee: 1,007 km (625 mi). Perigee: 971 km (603 mi). Inclination: 83.00 deg. Period: 104.90 min. Military navigation satellite..

1976 July 29

20:03 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 846 - . Mass: 650 kg (1,430 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 9061 . COSPAR: 1976-078A. Apogee: 1,009 km (626 mi). Perigee: 947 km (588 mi). Inclination: 82.90 deg. Period: 104.70 min. Military navigation satellite..

1977 January 20

20:05 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 890 - . Mass: 700 kg (1,540 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 9737 . COSPAR: 1977-004A. Apogee: 1,016 km (631 mi). Perigee: 975 km (605 mi). Inclination: 83.00 deg. Period: 105.00 min. Military navigation satellite..

1977 October 28

16:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 962 - . Mass: 700 kg (1,540 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 10459 . COSPAR: 1977-107A. Apogee: 1,006 km (625 mi). Perigee: 962 km (597 mi). Inclination: 83.00 deg. Period: 104.80 min. Military navigation satellite..

1978 March 15

15:57 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 994 - . Mass: 920 kg (2,020 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 10731 . COSPAR: 1978-028A. Apogee: 1,007 km (625 mi). Perigee: 971 km (603 mi). Inclination: 82.90 deg. Period: 104.90 min. Military navigation satellite..

1978 July 27

04:49 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 1027 - . Mass: 920 kg (2,020 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Tsiklon satellite. USAF Sat Cat: 10991 . COSPAR: 1978-074A. Apogee: 998 km (620 mi). Perigee: 957 km (594 mi). Inclination: 82.90 deg. Period: 104.70 min. Military navigation satellite..