Kh-23 Grom

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Explore the main themes, entities and connections around Kh-23 Grom. Start with the topic map, then use the sections below for research and deeper semantic analysis.

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Operators

North Korea Afghanistan Algeria Angola Azerbaijan

32 related topics

Development

Kaliningrad K-5 Su-9 OKB-4 Molniya Vympel NPO Matus Bisnovat

11 related topics

Variants

Kh-25 Polish SAM Military Technical Institute AGM-65B Maverick

4 related topics

Similar weapons

AS-20

1 related topics

Key facts & relationships

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.mw-parser-output .tooltip-dotted{border-bottom:1px dotted;cursor:help}Maximum speed: 2,160–2,700 km/h (1,340–1,680 mph)
Designer: Yurii N. Korolyov
Diameter: 27.5 cm (10.8 in)
Engine: Solid fuel rocket
Guidance system: Kh-66: Line-Of-Sight Beam riding Kh-23: Radio command guidance Grom-B: TV guidance
In service: Kh-66 :20 June 1968 Kh-23 :1973 Kh-23M :1974

Topics to explore

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Overview

Russian Russian language
NATO NATO reporting name
Soviet Soviet Union
Air-to-surface missiles Air-to-surface missile
K-8 (AA-3 'Anab') K-8 (missile)
AGM-12 Bullpup

Development

Variants

Operators

Similar weapons

AS-20

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

Nodes60

Edges59

Triples17

Avg. degree1.97

Density0.033333

Components1

How this topic connects Entity context

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Kh-23 Grom

Top relations

.mw-parser-output .tooltip-dotted{border-bottom:1px dotted;cursor:help}Maximum speed · 1

Kh-23 Grom → 2,160–2,700 km/h (1,340–1,680 mph)

Designer · 1

Kh-23 Grom → Yurii N. Korolyov

Diameter · 1

Kh-23 Grom → 27.5 cm (10.8 in)

Engine · 1

Kh-23 Grom → Solid fuel rocket

Guidance system · 1

Kh-23 Grom → Kh-66: Line-Of-Sight Beam riding Kh-23: Radio command guidance Grom-B: TV guidance

In service · 1

Kh-23 Grom → Kh-66 :20 June 1968 Kh-23 :1973 Kh-23M :1974

Launch platform · 1

Kh-23 Grom → Yak-38, MiG-21PFM, MiG-23, MiG-27, Su-17M3/20/22/22M3/M4,

Length · 1

Kh-23 Grom → A921 :3.525 m (11 ft 7 in)

Manufacturer · 1

Kh-23 Grom → Zvezda-Strela

Mass · 1

Kh-23 Grom → A921 :287 kg (633 lb)

Important terminology Word statistics

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Important terminology

kh-66 kh-23 missile soviet guidance service aircraft missiles beam-riding 1968 mig-23 air-to-surface entered family version k-8 air-to-air bullpup vietnam design

Entity relationships Subject–Predicate–Object triples

Subject	Predicate	Object	Confidence	Src
Kh-23 Grom	.mw-parser-output .tooltip-dotted{border-bottom:1px dotted;cursor:help}Maximum speed	2,160–2,700 km/h (1,340–1,680 mph)	1.00	infobox
Kh-23 Grom	Designer	Yurii N. Korolyov	1.00	infobox
Kh-23 Grom	Diameter	27.5 cm (10.8 in)	1.00	infobox
Kh-23 Grom	Engine	Solid fuel rocket	1.00	infobox
Kh-23 Grom	Guidance system	Kh-66: Line-Of-Sight Beam riding Kh-23: Radio command guidance Grom-B: TV guidance	1.00	infobox
Kh-23 Grom	In service	Kh-66 :20 June 1968 Kh-23 :1973 Kh-23M :1974	1.00	infobox
Kh-23 Grom	Launch platform	Yak-38, MiG-21PFM, MiG-23, MiG-27, Su-17M3/20/22/22M3/M4,	1.00	infobox
Kh-23 Grom	Length	A921 :3.525 m (11 ft 7 in)	1.00	infobox
Kh-23 Grom	Manufacturer	Zvezda-Strela	1.00	infobox
Kh-23 Grom	Mass	A921 :287 kg (633 lb)	1.00	infobox
Kh-23 Grom	Operational range	2–10 km (1.1–5.4 nmi)	1.00	infobox
Kh-23 Grom	Place of origin	Soviet Union	1.00	infobox
Kh-23 Grom	Type	Tactical air-to-surface missile	1.00	infobox
Kh-23 Grom	Used by	FSU, Warsaw Pact, Iraq, India	1.00	infobox
Kh-23 Grom	Warhead weight	111 kg (245 lb)	1.00	infobox
Kh-23 Grom	Wingspan	78.5 cm (2 ft 6.9 in)	1.00	infobox

Related concept clusters Concept neighborhoods

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Connections between topic areas Semantic bridges

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