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DS-U2-IK

Spacecraft · Ukraine

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

DS-U2-IK-1
DS-U2-IK-1
Credit: Yuzhnoye

Ukrainian earth ionosphere satellite. Studied charged particle flows and the ionosphere; version used for Intercosmos international launches.

East European experiments studied protons, electrons, alpha particles.

Design work began in April 1967. Adaptation of DS satellites by KB Yuzhnoye. For the Interkosmos modifications V F Chutkin was Chief Designer and First Assistant was V S Budnik.

More at: Interkosmos-3.

Country
Ukraine
Agency
IK, Yuzhnoye
Bibliography
116, 2, 6, 99, 12279

Chronology

8 events

1967 April

  • Design work begins on Interkosmos version of DS - . Nation: Russia. Spacecraft: DS-U1-IK, DS-U2-IK. For the Interkosmos modifications V F Chutkin was Chief Designer and First Assistant was V S Budnik. East European experiments studied protons, electrons, alpha particles..

1970 August 7

02:59 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC86/4. LV Family: R-12. Launch Vehicle: Kosmos 11K63.
  • Intercosmos 3 - . Payload: DS-U2-IK s/n 1. Mass: 340 kg (740 lb). Nation: Russia. Agency: MO. Program: DS. Class: Earth. Type: Ionosphere satellite. Spacecraft Bus: DS. Spacecraft: DS-U2-IK. Completed Operations Date: 1970-12-04 . Decay Date: 1970-12-06 . USAF Sat Cat: 4482 . COSPAR: 1970-057A. Apogee: 1,294 km (804 mi). Perigee: 201 km (124 mi). Inclination: 48.40 deg. Period: 99.80 min. Studied charged particle flows and the ionosphere. Carried East European experiments that studied protons, electrons, alpha particles..

1971 December 2

08:25 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC86/4. LV Family: R-12. Launch Vehicle: Kosmos 11K63.
  • Intercosmos 5 - . Payload: DS-U2-IK s/n 2. Mass: 340 kg (740 lb). Nation: Russia. Agency: IK. Program: DS. Class: Earth. Type: Ionosphere satellite. Spacecraft Bus: DS. Spacecraft: DS-U2-IK. Decay Date: 1972-04-07 . USAF Sat Cat: 5641 . COSPAR: 1971-104A. Apogee: 1,181 km (733 mi). Perigee: 198 km (123 mi). Inclination: 48.40 deg. Period: 98.50 min.

    Carried Czech and Soviet instruments that investigated the effects of solar activity on near-Earth radiation. Studied the radiation levels in near-Earth space, investigated dipole corpuscular streams in near space in connexion with solar activity and investigation of the nature and spectrum of low-frequency electromagnetic oscillations in natural plasma.

1973 April 19

10:19 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC86/4. LV Family: R-12. Launch Vehicle: Kosmos 11K63.
  • Intercosmos 9 - . Payload: DS-U2-IK s/n . Mass: 400 kg (880 lb). Nation: Russia. Agency: IK. Program: DS. Class: Earth. Type: Ionosphere satellite. Spacecraft Bus: DS. Spacecraft: DS-U2-IK. Completed Operations Date: 1973-10-15 . Decay Date: 1973-10-15 . USAF Sat Cat: 6433 . COSPAR: 1973-022A. Apogee: 1,526 km (948 mi). Perigee: 199 km (123 mi). Inclination: 48.40 deg. Period: 102.20 min. Also designated Intercosmos Copernicus 500. Investigated solar radio-frequency radiation and the characteristics of the earth's ionosphere..

1973 October 30

19:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Intercosmos 10 - . Payload: DS-U2-IK s/n 3. Mass: 550 kg (1,210 lb). Nation: Russia. Agency: IK. Program: DS. Class: Earth. Type: Ionosphere satellite. Spacecraft Bus: DS. Spacecraft: DS-U2-IK. Completed Operations Date: 1974-06-07 . Decay Date: 1977-07-01 . USAF Sat Cat: 6911 . COSPAR: 1973-082A. Apogee: 1,453 km (902 mi). Perigee: 257 km (159 mi). Inclination: 74.00 deg. Period: 102.00 min. Geophysical research at high latitudes to study the electromagnetic coupling of the earth's magnetosphere and ionosphere..

1974 October 31

10:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Intercosmos 12 - . Payload: DS-U2-IK s/n 4. Mass: 400 kg (880 lb). Nation: Russia. Agency: IK. Program: DS. Class: Earth. Type: Ionosphere satellite. Spacecraft Bus: DS. Spacecraft: DS-U2-IK. Completed Operations Date: 1975-02-20 . Decay Date: 1975-07-11 . USAF Sat Cat: 7500 . COSPAR: 1974-086A. Apogee: 707 km (439 mi). Perigee: 243 km (150 mi). Inclination: 74.00 deg. Period: 94.10 min. Atmospheric, ionospheric research. Comprehensive investigation of the earth's atmosphere and ionosphere and of micrometeorite fluxes..

1975 March 27

14:30 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Intercosmos 13 - . Payload: DS-U2-IK s/n 5. Mass: 400 kg (880 lb). Nation: Russia. Agency: IK. Program: DS. Class: Earth. Type: Ionosphere satellite. Spacecraft Bus: DS. Spacecraft: DS-U2-IK. Completed Operations Date: 1975-06-21 . Decay Date: 1980-09-02 . USAF Sat Cat: 7710 . COSPAR: 1975-022A. Apogee: 1,689 km (1,049 mi). Perigee: 284 km (176 mi). Inclination: 83.00 deg. Period: 104.90 min. Upper atmospheric experiments. Study of dynamic processes in the earth's magnetosphere and polar ionosphere and investigation of low-frequency electromagnetic waves..

1975 December 11

17:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Intercosmos 14 - . Payload: DS-U2-IK s/n 6. Mass: 700 kg (1,540 lb). Nation: Russia. Agency: IK. Program: DS. Class: Earth. Type: Ionosphere satellite. Spacecraft Bus: DS. Spacecraft: DS-U2-IK. Completed Operations Date: 1976-07-09 . Decay Date: 1983-02-27 . USAF Sat Cat: 8471 . COSPAR: 1975-115A. Apogee: 1,684 km (1,046 mi). Perigee: 335 km (208 mi). Inclination: 74.00 deg. Period: 105.30 min. Study of low-frequency electromagnetic vibrations in the magnetosphere of the earth, of the structure of the ionosphere and of the intensity of micrometeorite fluxes..