UR-100

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Explore the main themes, entities and connections around UR-100. Start with the topic map, then use the sections below for research and deeper semantic analysis.

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Operational history

Strategic Rocket Forces LGM-30 Minuteman 53rd Rocket Army 29th Arsenal

4 related topics

Description

Yield MIRV UR-100N UR-100MR

4 related topics

Overview

Russian Intercontinental ballistic missile Soviet Union Universal Rocket Cold War

11 related topics

Key facts & relationships

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Accuracy: 1000–1400 metres CEP
Blast yield: 1 Mt by NII-1011, Chelyabinsk-70
Diameter: 2,000 mm
Engine: first stage 8S816 with a 15D2 module (three RD-0216 and one RD-0217 engines) · second stage 8S817 with one 15D13 main and one four-nozzle 15D14 (RK-3) engines)
Guidance system: inertial
In service: 21 July 1967 (document №705-235)–1974

Topics to explore

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Overview

Russian Russian language
Intercontinental ballistic missile
Soviet Union
Universal Rocket
Cold War
NATO reporting name
Sego Calochortus nuttallii
GRAU
Strela Strela rocket
Rokot
MR-UR-100 Sotka (SS-17 Spanker) SS-17 Spanker

Description

Yield Nuclear weapon yield
MIRV
UR-100N
UR-100MR MR-UR-100 Sotka

Operational history

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

Nodes23

Edges22

Triples41

Avg. degree1.91

Density0.086957

Components1

How this topic connects Entity context

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UR-100

Top relations

related to Description · 16

UR-100 → Barmin, Common Machinery, Design Bureau, Facilities, Gerasimenko, ICBM, Initial, KBOM, MIRV, Mt, NII-108, October, Palma, The, The UR-100, This

related to Variants and developments · 9

UR-100 → Rokot, Russian, The, This, UR-100MR, UR-100N, UR-100N UTTH, UTTH, UTTKh

Engine · 2

UR-100 → first stage 8S816 with a 15D2 module (three RD-0216 and one RD-0217 engines), second stage 8S817 with one 15D13 main and one four-nozzle 15D14 (RK-3) engines)

related to As a space launcher · 2

UR-100 → Rokot, The Strela

Accuracy · 1

UR-100 → 1000–1400 metres CEP

Blast yield · 1

UR-100 → 1 Mt by NII-1011, Chelyabinsk-70

Diameter · 1

UR-100 → 2,000 mm

Guidance system · 1

UR-100 → inertial

In service · 1

UR-100 → 21 July 1967 (document №705-235)–1974

Length · 1

UR-100 → 16,930 mm

Important terminology Word statistics

Use these terms to understand the vocabulary surrounding the topic, not as a checklist for keyword stuffing.

Important terminology

russian missile icbm strela rokot 8k84 soviet rockets designation ur-100mr union operational citation needed improved rocket carrier based different yield

Entity relationships Subject–Predicate–Object triples

Subject	Predicate	Object	Confidence	Src
UR-100	Accuracy	1000–1400 metres CEP	1.00	infobox
UR-100	Blast yield	1 Mt by NII-1011, Chelyabinsk-70	1.00	infobox
UR-100	Diameter	2,000 mm	1.00	infobox
UR-100	Engine	first stage 8S816 with a 15D2 module (three RD-0216 and one RD-0217 engines)	1.00	infobox
UR-100	Engine	second stage 8S817 with one 15D13 main and one four-nozzle 15D14 (RK-3) engines)	1.00	infobox
UR-100	Guidance system	inertial	1.00	infobox
UR-100	In service	21 July 1967 (document №705-235)–1974	1.00	infobox
UR-100	Length	16,930 mm	1.00	infobox
UR-100	Manufacturer	design by OKB-52 of V.N.Chelomey, production by Khrunichev Machine-Building Plant, Omsk aviation facility №166 "Polyot", Orenburg aviation facility №47 "Strela"	1.00	infobox
UR-100	Mass	41.4-42.3 tonnes	1.00	infobox
UR-100	Operational range	10,600 km	1.00	infobox
UR-100	Type	ICBM	1.00	infobox
UR-100	Used by	Soviet Union	1.00	infobox
UR-100	Warhead	1	1.00	infobox

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