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Yantar-1KFT
Part of Yantar
Yantar 1K
Yantar 1K
Russian military surveillance satellite. Version of the Yantar photo satellite for topographic mapping on behalf of the Red Army. Area Reconnaissance, photo (film return type) satellite built by TsSKB for GRU, Russia. Launched 1981 - 2005. Used Yantar Bus, Zenit reentry module.

AKA: 11F660;Kometa;Siluet;Spin-2. Status: Operational 1981. First Launch: 1981-02-18. Last Launch: 2005-09-02. Number: 21 . Gross mass: 6,600 kg (14,500 lb).

The Yantar-1KF system was intended to build up high precision maps based on information from the Zenit-4MT. However it became impossible to keep the spacecraft within the weight that the Soyuz-U launch vehicle could lift. It would require a Proton or Zenit vehicle. Therefore the spacecraft was cancelled.

A complete design revision beginning in 1973 led to a production version of the Yantar photo satellite for topographic mapping for the Army General Staff. The revised satellite was developed in accordance with a resolution of 3 February 1977. Camera development began in the 1980's and flight trials began in 1981. The Yantar-1KFT was equipped with the Yakhont-1 TK-350 topographic camera and an APO-Oktan-8 objective, a product of the Byelorussia Optical Camera Company. These provided a focal length of 350 mm, with photo negative size of 300 x 450 mm, covering an area of 200 x 300 km with a resolution of 10 m and a scale of 1:660,000. The camera was designed for exceptional geometric precision for cartographic purposes and each image overlapped the next by 60% to 80% to allow stereoscopic pairs to be made. Closeup images were made by the KVR-1000 camera with a focal length of 1000 mm, a negative size of 180 x 180 mm covering an area of 40 km x 40 km at 1:50,000 scale and 2 m resolution. Western description: Fourth generation topographic. Typical orbital profile: inclination 64.9 degrees with an altitude of 207-270 km. Designed duration: 40 days. First flight: Cosmos 1246. Last flight: Cosmos 2284. Transmission frequencies observed in West: 150.3 PCM-FM; 400.8 CW.


More at: Yantar-1KFT.

Family: Military surveillance sat, Surveillance, Surveillance orbit. Country: Russia. Launch Vehicles: R-7, Soyuz 11A511, Soyuz-U, Soyuz-U-PVB. Launch Sites: Baikonur, Baikonur LC1, Baikonur LC31. Agency: MOM, Kozlov bureau. Bibliography: 101, 102, 110, 2, 276, 445, 474, 552, 554, 6, 13362.
Photo Gallery

Yantar multi-return Yantar multi-return
Yantar bus reconnaissance satellite with multiple re-entry capsules. This is believed to be layout of Orlets-1. Orlets-2 must have a considerably extended bus to accommodate even more capsules.


KometaKometa
Credit: Manufacturer Image



1971 March 26 - . LV Family: R-7. Launch Vehicle: Soyuz 11A511.
1976 May 31 - .
1981 February 18 - . 09:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-U.
1982 May 28 - . 09:10 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz-U.
1983 December 27 - . 09:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC31. LV Family: R-7. Launch Vehicle: Soyuz-U.
1984 November 14 - . 07:40 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz-U.
1985 August 8 - . 10:19 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz-U.
1986 October 6 - . 07:40 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
1987 July 8 - . 10:59 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
1987 November 14 - . 09:29 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
1988 May 18 - . 10:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
1988 December 29 - . 10:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
1989 May 24 - . 10:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
1990 May 15 - . 09:55 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
1991 February 15 - . 09:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1/LC31?. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
1991 December 17 - . 11:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
1992 April 29 - . 10:10 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
1993 April 27 - . 10:35 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
1994 July 29 - . 09:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
1996 May 14 - . 08:55 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB. FAILURE: Shroud broke up at T+49 seconds.. Failed Stage: S.
1998 February 17 - . 10:35 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
2000 September 29 - . 09:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
2005 September 2 - . 09:50 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.

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