Universal Rocket Module

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Overview

Liquid fuelled Angara Expendable launch system Soyuz-2 RD-191

16 related topics

Key facts & relationships

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Burn time: Angara 1.2: 214 s Angara A5 Booster: 214 s Angara A5 Core: 325 s
Country of origin: Russia
Diameter: 2.9 m (9 ft 6 in)
Gross mass: 142,400 kg (313,900 lb)
Height: 25.7 m (84 ft)
Manufacturer: Khrunichev

Topics to explore

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Overview

Liquid fuelled Liquid rocket
Angara Angara (rocket family)
Expendable launch system
Soyuz-2 Soyuz-2 (rocket)
RD-191
RP-1
Liquid oxygen
MN Newton (unit)
Angara 1.2PP Angara-1.2pp
Angara 1.2
Angara A5
RD-0124
Naro-1
Launch vehicle
Republic of Korea South Korea
KARI Korea Aerospace Research Institute

Advanced semantic analysis

Deeper signals for content research, entity SEO and topical coverage. The plain-language headings explain what each technical view is useful for.

Map overview Semantic statistics

Nodes18

Edges17

Triples12

Avg. degree1.89

Density0.111111

Components1

How this topic connects Entity context

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Universal Rocket Module

Top relations

Burn time · 1

Universal Rocket Module → Angara 1.2: 214 s Angara A5 Booster: 214 s Angara A5 Core: 325 s

Country of origin · 1

Universal Rocket Module → Russia

Diameter · 1

Universal Rocket Module → 2.9 m (9 ft 6 in)

Gross mass · 1

Universal Rocket Module → 142,400 kg (313,900 lb)

Height · 1

Universal Rocket Module → 25.7 m (84 ft)

Manufacturer · 1

Universal Rocket Module → Khrunichev

Maximum thrust · 1

Universal Rocket Module → 1,920 kN (430,000 lbf) (sea level)

Powered by · 1

Universal Rocket Module → 1 RD-191

Propellant · 1

Universal Rocket Module → LOX/Kerosene

Propellant mass · 1

Universal Rocket Module → 132,600 kg (292,300 lb)

Important terminology Word statistics

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Important terminology

angara stage urm-1 second first urm-2 block diameter rd-191 meters 2pp thrust a5 powered liquid booster core launch derived length

Entity relationships Subject–Predicate–Object triples

Subject	Predicate	Object	Confidence	Src
Universal Rocket Module	Burn time	Angara 1.2: 214 s Angara A5 Booster: 214 s Angara A5 Core: 325 s	1.00	infobox
Universal Rocket Module	Country of origin	Russia	1.00	infobox
Universal Rocket Module	Diameter	2.9 m (9 ft 6 in)	1.00	infobox
Universal Rocket Module	Gross mass	142,400 kg (313,900 lb)	1.00	infobox
Universal Rocket Module	Height	25.7 m (84 ft)	1.00	infobox
Universal Rocket Module	Manufacturer	Khrunichev	1.00	infobox
Universal Rocket Module	Maximum thrust	1,920 kN (430,000 lbf) (sea level)	1.00	infobox
Universal Rocket Module	Powered by	1 RD-191	1.00	infobox
Universal Rocket Module	Propellant	LOX/Kerosene	1.00	infobox
Universal Rocket Module	Propellant mass	132,600 kg (292,300 lb)	1.00	infobox
Universal Rocket Module	Specific impulse	311 seconds (3.05 km/s) (sea level)	1.00	infobox
Universal Rocket Module	Used on	Angara stage 1 and boosters	1.00	infobox

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