Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
DS-P1
Part of DS
DS-P1 Credit: Yuzhnoye |
Ukrainian military target satellite. Prototype ABM radar target; supported developmental experiments for ABM systems. Radar calibration satellite built by Yuzhnoye, Russia. Launched 1962 - 1964.
Status: Operational 1962. First Launch: 1962-06-30. Last Launch: 1964-02-27. Number: 4 . Gross mass: 355 kg (782 lb).
Developed by V M Kovtunenko at OKB-586. DS-type control-test complexes were used for radar tests of the PVO (Soviet Air Defense Forces). As a result of flight test of the DS-P1 in 1962 the practical use of this method was shown. The DS-P1 spacecraft used solar cells for the first time in a Yuzhnoye satellite. The cells were arranged around a dodecahedron that enclosed and was rigidly connected to the main sealed container portion of the satellite..
More at: DS-P1.
Family:
ABM target.
Country:
Ukraine.
Launch Vehicles:
Kosmos 2,
R-12,
Kosmos 63S1.
Launch Sites:
Kapustin Yar,
Kapustin Yar Mayak-2.
Agency:
MO,
Yuzhnoye.
Bibliography:
2,
445,
6,
99,
12265.
Photo Gallery
| DS-P1 s/n 2 Credit: Manufacturer Image |
1962 June 30 - .
16:00 GMT - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar Mayak-2.
LV Family:
R-12.
Launch Vehicle:
Kosmos 63S1.
- Cosmos 6 - .
Payload: DS-P1 s/n 1. Mass: 355 kg (782 lb). Nation: Russia.
Agency: RVSN.
Program: DS.
Class: Military.
Type: Military target satellite. Spacecraft Bus: DS.
Spacecraft: DS-P1.
Completed Operations Date: 1962-07-06 . Decay Date: 1962-09-08 . USAF Sat Cat: 338 . COSPAR: 1962-A-Delta-1. Apogee: 348 km (216 mi). Perigee: 261 km (162 mi). Inclination: 48.90 deg. Period: 90.60 min. Prototype ABM radar target; supported developmental experiments for ABM systems..
1963 April 6 - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar Mayak-2.
LV Family:
R-12.
Launch Vehicle:
Kosmos 63S1.
FAILURE: First stage failed..
Failed Stage: 1.
- DS-P1 s/n 2 - .
Payload: DS-P1. Mass: 355 kg (782 lb). Nation: Russia.
Agency: RVSN.
Program: DS.
Class: Military.
Type: Military target satellite. Spacecraft Bus: DS.
Spacecraft: DS-P1.
Prototype ABM radar target; supported developmental experiments for ABM systems..
1963 August 6 - .
06:00 GMT - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar Mayak-2.
LV Family:
R-12.
Launch Vehicle:
Kosmos 63S1.
- Cosmos 19 - .
Payload: DS-P1 s/n 3. Mass: 355 kg (782 lb). Nation: Russia.
Agency: MO.
Program: DS.
Class: Military.
Type: Military target satellite. Spacecraft Bus: DS.
Spacecraft: DS-P1.
Completed Operations Date: 1964-03-29 . Decay Date: 1964-03-30 . USAF Sat Cat: 632 . COSPAR: 1963-033A. Apogee: 497 km (308 mi). Perigee: 267 km (165 mi). Inclination: 49.00 deg. Period: 92.10 min. Prototype ABM radar target; supported developmental experiments for ABM systems..
1964 February 27 - .
13:26 GMT - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar Mayak-2.
LV Family:
R-12.
Launch Vehicle:
Kosmos 63S1.
- Cosmos 25 - .
Payload: DS-P1 s/n 4. Mass: 355 kg (782 lb). Nation: Russia.
Agency: MO.
Program: DS.
Class: Military.
Type: Military target satellite. Spacecraft Bus: DS.
Spacecraft: DS-P1.
Completed Operations Date: 1964-11-21 . Decay Date: 1964-11-21 . USAF Sat Cat: 757 . COSPAR: 1964-010A. Apogee: 495 km (307 mi). Perigee: 260 km (160 mi). Inclination: 49.10 deg. Period: 92.10 min. Prototype ABM radar target; supported developmental experiments for ABM systems..
Back to top of page
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2019 Mark Wade - Contact
© / Conditions for Use