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The N1 (from Ракета-носитель Raketa-nositel', "Carrier Rocket"; Cyrillic: Н1, GRAU index: 11A52, Sheldon: G-1-e, DoD: SL-15) was a super heavy-lift launch vehicle of the Soviet space program intended for crewed travel to the Moon and beyond. All four launch attempts between 1969 and 1972 failed. Studied and designed by OKB-1 since 1959, it was the…
The analysis highlights History, Launch history and Description as prominent areas in the source structure around N1 (rocket). 1 topic appears in more than one source area, which can help identify connections that are less obvious in a linear reading.
Source areas are shown by the number of related topics found in each part of the analysis. Use smaller areas too: they can reveal specialized angles and content gaps.
Smaller areas are not necessarily less important. They contain fewer connections in this analysis and can be useful for finding specialized angles or coverage gaps.
High-confidence facts extracted from structured source data. Use them as anchors for further research.
Browse the complete topic structure, not only the most central items. Less prominent entities and concepts can reveal missing angles, specialized context and useful research gaps. Each item opens a new analysis centered on that subject.
Deeper signals for content research, entity SEO and topical coverage. The plain-language headings explain what each technical view is useful for.
The extracted context around N1 (rocket) shows recurring relationship patterns in the source. For example, 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) Another extracted example is N1 (rocket) → 120 seconds, 125 seconds, 370 seconds, 443 seconds, 600 seconds. Use these groups to spot repeated connection types before inspecting the individual relationships.
Use these terms to understand the vocabulary surrounding the topic, not as a checklist for keyword stuffing.
engines launch n1 block rocket first engine stage lunar system moon soyuz would shut stages kord saturn soviet two korolev
TTTA extracted 43 structured relationships around N1 (rocket). Examples in this analysis include N1 (rocket) → Burn time → 125 seconds and N1 (rocket) → Burn time → 120 seconds. The table shows each extracted connection, where it came from and its confidence.
| 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 |
The concept neighborhoods around N1 (rocket) bring nearby vocabulary together. In this analysis, examples include Saturn, Launch and First. Use the clusters to find adjacent concepts and terminology that may deserve separate research.
For N1 (rocket), one of the stronger structural bridges in this analysis connects N1 (rocket) with History. Bridges highlight paths between different parts of the map and can reveal research angles that are easy to miss in a flat list.
TTTA analyzes the structure around N1 (rocket) to surface related topics, entities, relationships, concept neighborhoods and bridge connections. Use the map to explore areas such as History, Launch history & Description, including less central topics that may reveal useful research gaps. Automatically extracted connections are research leads rather than rewritten encyclopedia content.
Source: Wikipedia — N1 (rocket) · EN edition · Analysis: TopicsToTalkAbout