Tsyklon-3
From Wikipedia, the free encyclopedia
A Tsyklon-3 launching a Meteor-3 satellite |
|
| Function | Carrier rocket |
|---|---|
| Manufacturer | Yuzhmash |
| Country of origin | Soviet Union (Ukraine) |
| Size | |
| Height | 39.27 m (128.83 ft) |
| Diameter | 3 m (9.8 ft) |
| Mass | 189,000 kg (416,000 lb) |
| Stages | 3 |
| Capacity | |
| Payload to LEO | 4,100 kg (9,000 lb) |
| Associated rockets | |
| Family | R-36, Tsyklon |
| Derivatives | Tsyklon-4 |
| Comparable | Delta II |
| Launch history | |
| Status | Retired[1] |
| Launch sites | Plesetsk Cosmodrome LC-32 |
| Total launches | 122 |
| Successes | 114 |
| Failures | 8 |
| First flight | 24 June 1977 |
| Last flight | 30 January 2009[1] |
| Notable payloads | Tselina Meteor Okean Geo-IK Strela |
| First Stage - 11K69 | |
| Engines | 1 RD-261 |
| Thrust | 3,032 kN (681,620 lbf) |
| Specific impulse | 301 sec |
| Burn time | 120 seconds |
| Fuel | N2O4/UDMH |
| Second Stage - 11S692 | |
| Engines | 1 RD-262 |
| Thrust | 941 kN (211,545 lbf) |
| Specific impulse | 318 sec |
| Burn time | 160 seconds |
| Fuel | N2O4/UDMH |
| Third Stage - 11S693 | |
| Engines | 1 RD-861 |
| Thrust | 78.70 kN (17,694 lbf) |
| Specific impulse | 317 sec |
| Burn time | 125 seconds |
| Fuel | N2O4/UDMH |
The Tsyklon-3, also known as Tsiklon-3, GRAU index 11K68, was a Soviet, and subsequently Ukrainian orbital carrier rocket. A derivative of the R-36 ICBM, and a member of the Tsyklon family, it made its maiden flight on 24 June 1977, and was retired on 30 January 2009.[1] The Ukrainian-built Tsyklon rockets were retired in favour of future all-Russian carrier rockets, such as the Angara, and because they were fuelled by toxic hypergolic propellants.[2]
Ukraine is developing a commercial derivative of the Tsyklon-3, the Tsyklon-4.
See also [edit]
External links [edit]
References [edit]
- ^ a b c Barbosa, Rui C. (2009-01-30). "Russian Tsyklon-3 bows out with CORONAS launch". NASASpaceflight.com. Retrieved 2009-01-30.
- ^ APMC - Космические войска обеспечили реальность сроков сдачи в эксплуатацию перспективного РКК "Ангара" (Russian)
|
||||||||||||||
|
|||||||||||
| This rocketry article is a stub. You can help Wikipedia by expanding it. |