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astronautix.com Rokot

Rokot
Rokot -

Credit: Khrunichev. 20,162 bytes. 14 x 101 pixels.



Family: UR. Country: Russia. Status: Hardware. Other Designations: RS-18. Department of Defence Designation: SS-19 Mod.1. Article Number: 15A30. Manufacturer's Designation: UR-100N.

Launch vehicle based decommissioned Chelomei ICBMs. 106 tonne liftoff mass.


Specifications

Launches: 4. Failures: 0. Success Rate: 100.00% pct. First Launch Date: 20 December 1990. Last Launch Date: 16 May 2000. LEO Payload: 1,800 kg. to: 200 km Orbit. at: 53.0 degrees. Payload: 1,000 kg. to a: sun synchronous, 800 km, 98.6 deg orbital trajectory. Liftoff Thrust: 190,000 kgf. Total Mass: 107,000 kg. Core Diameter: 2.5 m. Total Length: 29.1 m. Launch Price $: 15.00 million. in 1999 price dollars.


Rokot Chronology


1990 Dec 20 - LV Configuration: Rokot (2 stage). Launch Site: Baikonur .
1991 Dec 20 - Launch Site: Baikonur .
1994 Dec 26 - - 03:01 GMT. Launch Site: Baikonur . Launch Complex: LC175.
2000 May 16 - - 08:27 GMT. Launch Site: Plesetsk .

Bibliography:



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Last update 12 March 2001.
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