Nuri (rocket)

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Explore the main themes, entities and connections around Nuri (rocket). Start with the topic map, then use the sections below for research and deeper semantic analysis.

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Development

Expendable Medium-lift Launch vehicle Hanwha Techwin Combustion instability

10 related topics

History

Sun-synchronous orbit Medium-sized liquid-propellant rocket

2 related topics

Overview

Korean Three-stage-to-orbit Small-lift launch vehicle South Korea Naro-1

15 related topics

Specification

Specific impulse Jet A Liquid oxygen

3 related topics

Key facts & relationships

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Altitude: 200 km (120 mi) · 700 km (430 mi)
Burn time: 127 seconds · 148 seconds · 498 seconds
Country of origin: South Korea
Diameter: 3.5 m (11 ft) · 2.6 m (8 ft 6 in)
Failure: 1
First flight: 21 October 2021

Topics to explore

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Overview

History

Sun-synchronous orbit
Medium-sized liquid-propellant rocket Liquid-propellant rocket

Specification

Development

Expendable Expendable launch system
Medium-lift Medium-lift launch vehicle
Launch vehicle
Hanwha Techwin
Combustion instability
Ground test Rocket engine test facility
Liquid rocket propellant
Ministry of Science and ICT
South Korea Ballistic Missile Range Guidelines
KSLV-III

Usage

Earth observation satellites Earth observation satellite
KOMPSAT
Southeast Asia

Advanced semantic analysis

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Map overview Semantic statistics

Nodes39

Edges38

Triples41

Avg. degree1.95

Density0.051282

Components1

How this topic connects Entity context

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Nuri (rocket)

Top relations

Manufacturer · 4

Nuri (rocket) → Hanwha Aerospace (engine manufacturing), Hyundai Heavy Industries (launchpad), Korea Aerospace Industries (final assembly), Korea Aerospace Research Institute (design)

Mass · 4

Nuri (rocket) → 1,000 kg (2,200 lb), 1,900 kg (4,200 lb), 200,000 kg (440,000 lb), 3,300 kg (7,300 lb)

Burn time · 3

Nuri (rocket) → 127 seconds, 148 seconds, 498 seconds

Height · 3

Nuri (rocket) → 21.6 m (71 ft), 3.5 m (11 ft), 47.2 m (155 ft)

Maximum thrust · 3

Nuri (rocket) → 68.7 kN (15,400 lbf), 788 kN (177,000 lbf), SL: 2,942 kN (661,000 lbf) vac: 3,380 kN (759,000 lbf)

Powered by · 3

Nuri (rocket) → 1 × KRE-007, 1 × KRE-075, 4 × KRE-075

Specific impulse · 3

Nuri (rocket) → 315.4 s (3.093 km/s), 325.1 s (3.188 km/s), SL: 261.7 s (2.566 km/s) vac: 298.6 s (2.928 km/s)

Altitude · 2

Nuri (rocket) → 200 km (120 mi), 700 km (430 mi)

Diameter · 2

Nuri (rocket) → 2.6 m (8 ft 6 in), 3.5 m (11 ft)

Country of origin · 1

Nuri (rocket) → South Korea

Important terminology Word statistics

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Important terminology

launch engine south nuri korea first vehicle seconds kre-075 korean second flight kslv-ii stage test developed tlv km rocket combustion

Entity relationships Subject–Predicate–Object triples

Subject	Predicate	Object	Confidence	Src
Nuri (rocket)	Altitude	200 km (120 mi)	1.00	infobox
Nuri (rocket)	Altitude	700 km (430 mi)	1.00	infobox
Nuri (rocket)	Burn time	127 seconds	1.00	infobox
Nuri (rocket)	Burn time	148 seconds	1.00	infobox
Nuri (rocket)	Burn time	498 seconds	1.00	infobox
Nuri (rocket)	Country of origin	South Korea	1.00	infobox
Nuri (rocket)	Diameter	3.5 m (11 ft)	1.00	infobox
Nuri (rocket)	Diameter	2.6 m (8 ft 6 in)	1.00	infobox
Nuri (rocket)	Failure	1	1.00	infobox
Nuri (rocket)	First flight	21 October 2021	1.00	infobox
Nuri (rocket)	Function	Small/Medium-lift launch vehicle	1.00	infobox
Nuri (rocket)	Height	47.2 m (155 ft)	1.00	infobox
Nuri (rocket)	Height	21.6 m (71 ft)	1.00	infobox
Nuri (rocket)	Height	3.5 m (11 ft)	1.00	infobox
Nuri (rocket)	Last flight	26 November 2025 (most recent)	1.00	infobox
Nuri (rocket)	Launch sites	Naro, LC-2	1.00	infobox
Nuri (rocket)	Manufacturer	Korea Aerospace Research Institute (design)	1.00	infobox
Nuri (rocket)	Manufacturer	Korea Aerospace Industries (final assembly)	1.00	infobox
Nuri (rocket)	Manufacturer	Hanwha Aerospace (engine manufacturing)	1.00	infobox
Nuri (rocket)	Manufacturer	Hyundai Heavy Industries (launchpad)	1.00	infobox
Nuri (rocket)	Mass	200,000 kg (440,000 lb)	1.00	infobox
Nuri (rocket)	Mass	3,300 kg (7,300 lb)	1.00	infobox
Nuri (rocket)	Mass	1,900 kg (4,200 lb)	1.00	infobox
Nuri (rocket)	Mass	1,000 kg (2,200 lb)	1.00	infobox
Nuri (rocket)	Maximum thrust	SL: 2,942 kN (661,000 lbf) vac: 3,380 kN (759,000 lbf)	1.00	infobox
Nuri (rocket)	Maximum thrust	788 kN (177,000 lbf)	1.00	infobox
Nuri (rocket)	Maximum thrust	68.7 kN (15,400 lbf)	1.00	infobox
Nuri (rocket)	Powered by	4 × KRE-075	1.00	infobox
Nuri (rocket)	Powered by	1 × KRE-075	1.00	infobox
Nuri (rocket)	Powered by	1 × KRE-007	1.00	infobox

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