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Dnepr (rocket)

The Dnepr rocket (Russian: Днепр, romanized: Dnepr; Ukrainian: Дніпро, romanized: Dnipró) was a space launch vehicle named after the Dnieper River. It was a converted ICBM used for launching artificial satellites into orbit, operated by launch service provider ISC Kosmotras. The first launch, on April 21, 1999, successfully placed UoSAT-12, a 350 kg…

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Based on
R-36M
Burn time
130 seconds · 190 seconds · 1,000 seconds
Cost per launch
US$29 million
Country of origin
Soviet Union (original build), Ukraine (commercial launches after 1999)
Diameter
3 m (9.8 ft)
Failure
1

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Dnepr (rocket)

Nodes45
Edges44
Triples36
Avg. degree1.96
Density0.044444
Components1

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Dnepr (rocket)

Top relations

Mass · 5
Dnepr (rocket) → 2,300 kilograms (5,100 lb), 211,000 kg (465,000 lb), 3,200 kilograms (7,100 lb), 4,500 kilograms (9,900 lb), 550 kilograms (1,210 lb) (with ST-1)
Burn time · 3
Dnepr (rocket) → 1,000 seconds, 130 seconds, 190 seconds
Manufacturer · 3
Dnepr (rocket) → Khartron (control system), Yuzhmash (manufacturing), Yuzhnoye Design Bureau (design)
Maximum thrust · 3
Dnepr (rocket) → 20.2 kN (4,500 lbf), 4,520 kN (1,020,000 lbf), 755 kN (170,000 lbf)
Powered by · 3
Dnepr (rocket) → 1 RD-0255 module (one RD-0256 main engine and one RD-0257 vernier), 1 RD-264 module (four RD-263 engines), 1 RD-864
Specific impulse · 3
Dnepr (rocket) → 309 s (3.03 km/s), 318 s (3.12 km/s), 340 s (3.3 km/s)
Propellant · 2
Dnepr (rocket) → .mw-parser-output .template-chem2-su{display:inline-block;font-size:80%;line-height:1;vertical-align:-0.35em}.mw-parser-output .template-chem2-suspan{display:block;text-align:l…, N2O4 / UDMH
Based on · 1
Dnepr (rocket) → R-36M
Cost per launch · 1
Dnepr (rocket) → US$29 million
Country of origin · 1
Dnepr (rocket) → Soviet Union (original build), Ukraine (commercial launches after 1999)

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Important terminology

launch dnepr rocket service orbit km icbm failure space vehicle used satellites kosmotras low commercial kg ukrainian russia converted isc

Entity relationships Subject–Predicate–Object triples

SubjectPredicateObjectConfidenceSrc
Dnepr (rocket)Based onR-36M1.00infobox
Dnepr (rocket)Burn time130 seconds1.00infobox
Dnepr (rocket)Burn time190 seconds1.00infobox
Dnepr (rocket)Burn time1,000 seconds1.00infobox
Dnepr (rocket)Cost per launchUS$29 million1.00infobox
Dnepr (rocket)Country of originSoviet Union (original build), Ukraine (commercial launches after 1999)1.00infobox
Dnepr (rocket)Diameter3 m (9.8 ft)1.00infobox
Dnepr (rocket)Failure11.00infobox
Dnepr (rocket)First flight21 April 19991.00infobox
Dnepr (rocket)FunctionOrbital carrier rocket1.00infobox
Dnepr (rocket)Height34.3 m (113 ft)1.00infobox
Dnepr (rocket)Last flight25 March 20151.00infobox
Dnepr (rocket)Launch sitesSite 109/95, Baikonur LC-13, Yasny1.00infobox
Dnepr (rocket)ManufacturerYuzhnoye Design Bureau (design)1.00infobox
Dnepr (rocket)ManufacturerYuzhmash (manufacturing)1.00infobox
Dnepr (rocket)ManufacturerKhartron (control system)1.00infobox
Dnepr (rocket)Mass211,000 kg (465,000 lb)1.00infobox
Dnepr (rocket)Mass4,500 kilograms (9,900 lb)1.00infobox
Dnepr (rocket)Mass3,200 kilograms (7,100 lb)1.00infobox
Dnepr (rocket)Mass2,300 kilograms (5,100 lb)1.00infobox
Dnepr (rocket)Mass550 kilograms (1,210 lb) (with ST-1)1.00infobox
Dnepr (rocket)Maximum thrust4,520 kN (1,020,000 lbf)1.00infobox
Dnepr (rocket)Maximum thrust755 kN (170,000 lbf)1.00infobox
Dnepr (rocket)Maximum thrust20.2 kN (4,500 lbf)1.00infobox
Dnepr (rocket)Powered by1 RD-264 module (four RD-263 engines)1.00infobox
Dnepr (rocket)Powered by1 RD-0255 module (one RD-0256 main engine and one RD-0257 vernier)1.00infobox
Dnepr (rocket)Powered by1 RD-8641.00infobox
Dnepr (rocket)Propellant.mw-parser-output .template-chem2-su{display:inline-block;font-size:80%;line-height:1;vertical-align:-0.35em}.mw-parser-output .template-chem2-su>span{display:block;text-align:l…1.00infobox
Dnepr (rocket)PropellantN2O4 / UDMH1.00infobox
Dnepr (rocket)Specific impulse318 s (3.12 km/s)1.00infobox

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