To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

4,5
Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.
.
Leo
Newton
Brights
Milds

From Wikipedia, the free encyclopedia

Tsyklon-4
FunctionCarrier rocket
Manufacturer
Country of originUkraine
Size
Height39.95 m (131.1 ft)
Diameter3.0 m (9.8 ft)
Mass198,250 kg (437,070 lb)
Stages3
Capacity
Payload to
Associated rockets
FamilyR-36 / Tsyklon
ComparableZenit
Launch history
StatusCancelled
Launch sitesAlcântara ACS Pad
First stage – 11K69
Engines1 × RD-261 + RD-855 Vernier engine
Thrust2,970 kN (303 tf)
Specific impulse300.4 s (2.946 km/s)
Burn time119 seconds
FuelN
2
O
4
/ UDMH
Second stage – 11S692
Engines1 × RD-262 + RD-856 Vernier engine
Thrust995 kN (101.5 tf)
Specific impulse314 s (3.08 km/s)
Burn time162 seconds
FuelN
2
O
4
/ UDMH
Third stage
Engines1 × RD-861K
Thrust76 kN (7.8 tf)
Specific impulse325 s (3.19 km/s)
Burn time450 seconds
FuelN
2
O
4
/ UDMH

The Tsyklon-4, also known as Tsiklon-4 and Cyclone-4, was a Ukrainian carrier rocket which was being developed for commercial satellite launches. Derived from the Tsyklon-3, it had a new third stage, a larger payload fairing, and a modernised flight control system compared to its predecessor.[1] The control system had been developed by JSC Khartron.[2][3]

Specifications

Tsyklon-4 was a three-stage-to-orbit expendable launch system, built on the successful Tsyklon-3 rocket and using improved versions of that rocket's first two stages. The new features were mostly in the newly developed third stage:

  • The third stage has three times the propellant capacity of Tsyklon-3
  • The new rocket engine RD-861K with multiple ignition capability (3 to 5 times)
  • A modern western-like control system capable of precise orbit injections
  • A new fairing derived from Ariane 4 is under development. It has a diameter of 4 metres (13 ft), with controlled temperature and cleanness conditions inside

Tsyklon-4 would have improved the fuelling system, allowing safe capture of toxic vapours from the vehicle's hypergolic propellant system.

The launch system would have been able to deliver up to 5,250 kg (11,570 lb) to a 185 km (115 mi) orbit, 4,900 kg (10,800 lb) to a 400 km (250 mi) orbit, or 500 kg (1,100 lb) to a geosynchronous orbit.[4]

Development history

Development began in 2002, with the maiden flight aimed for 2006. Following a series of production delays, this launch date slipped, and was estimated to occur some time after 2015.

Tsyklon-4 had been planned to launch from a proposed launch pad at the Alcântara Launch Center in Brazil, which would have given the rocket access to all orbital regimes. However, Brazil backed out of the partnership with Ukraine in 2015, citing concerns over the project budget, the ongoing financial situation in both countries, and the future of the commercial launch market.[5] Yuzhnoye began developing a two-stage derivative of Tsyklon-4, the Cyclone-4M, for Maritime Launch Services, a Canadian launch service provider. The new rocket was originally scheduled to be in service by 2020,[6][7] though this date has been repeatedly pushed due to construction delays at the Canso launch site. Construction is currently estimated to be complete by 2024 or 2025.[8]

See also

References

  1. ^ "Cyclone-4 Launch Vehicle". NPO InterCoS.
  2. ^ Control systems for intercontinental ballistic missiles and launch vehicles
  3. ^ Krivonosov, Khartron: Computers for rocket guidance systems
  4. ^ "Tsiklon-4". Encyclopedia Astronautica. Retrieved 8 August 2016. CS1 maint: discouraged parameter (link)
  5. ^ de Selding, Peter B. (16 April 2015). "Brazil Pulling Out of Ukrainian Cyclone-4 Launcher Project". Space News. Retrieved 9 April 2016.
  6. ^ Ruskin, Brett; Williams, Cassie (14 March 2017). "T-minus 1 year until rocket launch site construction starts in Nova Scotia". CBC News. Retrieved 18 March 2017. CS1 maint: discouraged parameter (link)
  7. ^ Boucher, Marc (14 March 2017). "Exclusive: Maritime Launch Services Selects Nova Scotia Site for Spaceport Over 13 Other Locations". SpaceQ. Retrieved 18 March 2017. CS1 maint: discouraged parameter (link)
  8. ^ Golubeva, Alena (9 April 2021). "Максим Дегтярев: «Спрос на выведение грузов на орбиту будет расти»" [Maxim Degtyarev: "The demand for placing cargo into orbit will grow"]. GMK Center (in Russian). Retrieved 11 May 2021. Компания получила разрешение, оформляет документы на получение земельного участка и уже в текущем году рассчитывает начать строительные работы. Сколько времени уйдет на строительство космодрома? – Три-четыре года. [The company has received permission, and is preparing documents for obtaining a land plot and expects to start construction work this year. How long will it take to build the cosmodrome? – Three or four years.]

External links

This page was last edited on 11 May 2021, at 08:06
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.