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Rokot

Rokot (Russian: Рокот meaning Rumble or Boom), also transliterated Rockot, was a Soviet Union (later Russian) space launch vehicle that was capable of launching a payload of 1,950 kilograms (4,300 lb) into a 200-kilometre (120 mi) Earth orbit with 63° inclination. It was based on the UR-100N (SS-19 Stiletto) intercontinental ballistic missile (ICBM)…

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Burn time
120 seconds · 180 seconds · 3,000 seconds
Cost per launch
US$41.8 million
Country of origin
Soviet Union
Diameter
2.5 m (8 ft 2 in)
Failure
2
First flight
20 November 1990 26 December 1994 (orbital)

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Overview

Specifications

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Rokot

Nodes43
Edges42
Triples72
Avg. degree1.95
Density0.046512
Components1

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Rokot

Top relations

related to history · 28
Rokot → Although, Arianespace, Astrium, Astrium GmbH, Baikonur, Baikonur Cosmodrome, December, Earth, Eurockot, Eurockot Launch Services, Eurockot's, Eurokot, German, German DaimlerBenz Aerospace, In, Khrunichev, Khrunichev State Research, Later, May, November
related to Specifications · 14
Rokot → All, Breeze-KM, Briz-KM, N2O4, RD-0233, RD-0234, RD-0235, Rokot's, Russian, Soviet UR-100N ICBM, SS-19, The, The Strela, UDMH
Burn time · 3
Rokot → 120 seconds, 180 seconds, 3,000 seconds
Mass · 3
Rokot → 1,200 kg (2,600 lb), 1,950 kg (4,300 lb), 107,000 kg (236,000 lb)
Maximum thrust · 3
Rokot → 19.6 kN (4,400 lbf), 2,080 kN (470,000 lbf), 255.76 kN (57,500 lbf)
Powered by · 3
Rokot → 1 RD-0235 (15D113) 1 RD-0236 (15D114), 1 S5.98M, 3 RD-0233 (15D95) 1 RD-0234 (15D96)
Specific impulse · 2
Rokot → 310 s (3.0 km/s), 326 s (3.20 km/s)
Cost per launch · 1
Rokot → US$41.8 million
Country of origin · 1
Rokot → Soviet Union
Diameter · 1
Rokot → 2.5 m (8 ft 2 in)

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Important terminology

launch space launches failure khrunichev first russian vehicle cosmodrome baikonur plesetsk state research production center soviet company later launching also

Entity relationships Subject–Predicate–Object triples

SubjectPredicateObjectConfidenceSrc
RokotBurn time120 seconds1.00infobox
RokotBurn time180 seconds1.00infobox
RokotBurn time3,000 seconds1.00infobox
RokotCost per launchUS$41.8 million1.00infobox
RokotCountry of originSoviet Union1.00infobox
RokotDiameter2.5 m (8 ft 2 in)1.00infobox
RokotFailure21.00infobox
RokotFirst flight20 November 1990 26 December 1994 (orbital)1.00infobox
RokotFunctionOrbital launch vehicle1.00infobox
RokotHeight29 m (95 ft)1.00infobox
RokotLast flight26 December 20191.00infobox
RokotLaunch sitesBaikonur, 175/1 Plesetsk, 133/31.00infobox
RokotManufacturerKhrunichev State Research and Production Space Center1.00infobox
RokotMass107,000 kg (236,000 lb)1.00infobox
RokotMass1,950 kg (4,300 lb)1.00infobox
RokotMass1,200 kg (2,600 lb)1.00infobox
RokotMaximum thrust2,080 kN (470,000 lbf)1.00infobox
RokotMaximum thrust255.76 kN (57,500 lbf)1.00infobox
RokotMaximum thrust19.6 kN (4,400 lbf)1.00infobox
RokotPartial failure11.00infobox
RokotPowered by3 RD-0233 (15D95) 1 RD-0234 (15D96)1.00infobox
RokotPowered by1 RD-0235 (15D113) 1 RD-0236 (15D114)1.00infobox
RokotPowered by1 S5.98M1.00infobox
RokotPropellantN2O4 / UDMH1.00infobox
RokotSpecific impulse310 s (3.0 km/s)1.00infobox
RokotSpecific impulse326 s (3.20 km/s)1.00infobox
RokotStages31.00infobox
RokotStatusRetired1.00infobox
RokotSuccess(es)311.00infobox
RokotTotal launches341.00infobox

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