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DS-U2-IK
Part of DS
|  DS-U2-IK-1
 Credit: Yuzhnoye
 | 
Ukrainian earth ionosphere satellite. Studied charged particle flows and the ionosphere; version used for Intercosmos international launches.
 Status: Operational 1970.  First Launch: 1970-08-07.  Last Launch: 1975-12-11.  Number:  7 . 
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. 
Family: 
Earth, 
Ionosphere sat. 
Country: 
Ukraine. 
Launch Vehicles: 
Kosmos 2, 
R-12, 
R-14, 
Kosmos 11K63, 
Kosmos 3, 
Kosmos 11K65M. 
Launch Sites: 
Kapustin Yar, 
Plesetsk, 
Plesetsk LC132/2, 
Kapustin Yar LC86/4, 
Plesetsk LC132/1. 
Agency: 
IK, 
Yuzhnoye. 
Bibliography: 
116, 
2, 
6, 
99, 
12279. 
Photo Gallery
|  | DS-U2-IK-2 Credit: Yuzhnoye
 | 
|  | DS-U2-IK-3 Credit: Yuzhnoye
 | 
|  | DS-U2-IK-4 Credit: Yuzhnoye
 | 
|  | DS-U2-IK-5 Credit: Yuzhnoye
 | 
|  | DS-U2-IK-6 Credit: Yuzhnoye
 | 
|  | DS-U2-IK-8 Credit: Yuzhnoye
 | 
|  | Intercosmos 3 Credit: Manufacturer Image
 | 
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.. 
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