N1 (rocket)

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Explore the main themes, entities and connections around N1 (rocket). Start with the topic map, then use the sections below for research and deeper semantic analysis.

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History

Race N1/L3 program Launch vehicle Apollo 4 Soviet Kazakhstan

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Launch history

Zond L1S-1 Voltage Pogo oscillation Launch escape system Sergei Afanasiev

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Description

Trans-lunar injection Frustum Grid fins Air-to-air missile Russian alphabet

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Overview

GRAU Sheldon DoD Super heavy-lift launch vehicle Soviet space program

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Key facts & relationships

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Burn time: 125 seconds · 120 seconds · 370 seconds · 443 seconds · 600 seconds
Comparable: Saturn V
Country of origin: USSR
Diameter: 17 m (56 ft)
Failure: 4
First flight: 21 February 1969

Topics to explore

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Bibliography

ISBN ISBN (identifier)

Advanced semantic analysis

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Map overview Semantic statistics

Nodes160

Edges159

Triples43

Avg. degree1.99

Density0.0125

Components1

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N1 (rocket)

Top relations

Maximum thrust · 6

N1 (rocket) → 1,800 kN (400,000 lbf), 14,064 kN (3,162,000 lbf), 329 kN (74,000 lbf), 83.36 kN (18,740 lbf), SL: 45,780 kN (10,290,000 lbf), vac: 46,320 kN (10,410,000 lbf)

Burn time · 5

N1 (rocket) → 120 seconds, 125 seconds, 370 seconds, 443 seconds, 600 seconds

Powered by · 5

N1 (rocket) → 1 × NK-21, 1 × RD-58, 30 × NK-15, 4 × NK-19, 8 × NK-15V

Specific impulse · 5

N1 (rocket) → 325 s (3.19 km/s), 346 s (3.39 km/s), 349 s (3.42 km/s), SL: 297 s (2.91 km/s), vac: 318 s (3.12 km/s)

Mass · 3

N1 (rocket) → 2,750,000 kg (6,060,000 lb), 95,000 kg (209,000 lb), cca 33,000 kg (73,000 lb)[a]

Comparable · 1

N1 (rocket) → Saturn V

Cost per launch · 1

N1 (rocket) → US$604 million in 1985 dollars ($1.81 billion in .mw-parser-output .tooltip-dotted{border-bottom:1px dotted;cursor:help}2025)

Country of origin · 1

N1 (rocket) → USSR

Diameter · 1

N1 (rocket) → 17 m (56 ft)

Failure · 1

N1 (rocket) → 4

Important terminology Word statistics

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Important terminology

engines launch n1 block rocket first engine stage lunar system moon soyuz would shut stages kord saturn soviet two korolev

Entity relationships Subject–Predicate–Object triples

Subject	Predicate	Object	Confidence	Src
N1 (rocket)	Burn time	125 seconds	1.00	infobox
N1 (rocket)	Burn time	120 seconds	1.00	infobox
N1 (rocket)	Burn time	370 seconds	1.00	infobox
N1 (rocket)	Burn time	443 seconds	1.00	infobox
N1 (rocket)	Burn time	600 seconds	1.00	infobox
N1 (rocket)	Comparable	Saturn V	1.00	infobox
N1 (rocket)	Cost per launch	US$604 million in 1985 dollars ($1.81 billion in .mw-parser-output .tooltip-dotted{border-bottom:1px dotted;cursor:help}2025)	1.00	infobox
N1 (rocket)	Country of origin	USSR	1.00	infobox
N1 (rocket)	Diameter	17 m (56 ft)	1.00	infobox
N1 (rocket)	Failure	4	1.00	infobox
N1 (rocket)	First flight	21 February 1969	1.00	infobox
N1 (rocket)	Function	Super heavy-lift launch vehicle for crewed lunar mission	1.00	infobox
N1 (rocket)	Height	105.3 m (345 ft)	1.00	infobox
N1 (rocket)	Last flight	23 November 1972	1.00	infobox
N1 (rocket)	Launch sites	Baikonur, Site 110	1.00	infobox
N1 (rocket)	Manufacturer	OKB-1	1.00	infobox
N1 (rocket)	Mass	2,750,000 kg (6,060,000 lb)	1.00	infobox
N1 (rocket)	Mass	95,000 kg (209,000 lb)	1.00	infobox
N1 (rocket)	Mass	cca 33,000 kg (73,000 lb)[a]	1.00	infobox
N1 (rocket)	Maximum thrust	SL: 45,780 kN (10,290,000 lbf)	1.00	infobox
N1 (rocket)	Maximum thrust	vac: 46,320 kN (10,410,000 lbf)	1.00	infobox
N1 (rocket)	Maximum thrust	14,064 kN (3,162,000 lbf)	1.00	infobox
N1 (rocket)	Maximum thrust	1,800 kN (400,000 lbf)	1.00	infobox
N1 (rocket)	Maximum thrust	329 kN (74,000 lbf)	1.00	infobox
N1 (rocket)	Maximum thrust	83.36 kN (18,740 lbf)	1.00	infobox
N1 (rocket)	Powered by	30 × NK-15	1.00	infobox
N1 (rocket)	Powered by	8 × NK-15V	1.00	infobox
N1 (rocket)	Powered by	4 × NK-19	1.00	infobox
N1 (rocket)	Powered by	1 × NK-21	1.00	infobox
N1 (rocket)	Powered by	1 × RD-58	1.00	infobox

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