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The LR91 was an American liquid-propellant rocket engine, which was used on the second stages of Titan intercontinental ballistic missiles and launch vehicles. While the original version - the LR91-3 - ran on RP-1/LOX (as did the companion LR87-3) on the Titan I, the models that propelled the Titan II and later were switched to Aerozine 50/N2O4.
The analysis highlights Products, Overview and Versions as prominent areas in the source structure around LR91.
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.
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The extracted context around LR91 shows recurring relationship patterns in the source. For example, LR91 → Aerozine, Gemini Titan II, LR91-11, LR91-3, LR91-5, LR91-5LR91-7LR91-11, LR91-7, LR91-9, N2O4, Propellant, RP-1/LOX, Run, Similar, Stage, Titan, Titan II, Titan III, Titan IV, Used, Version Another extracted example is LR91 → Upper stage. 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.
titan used ii version engine rp-1 stage n2o4 aerozine 50 gas-generator missiles launch ran liquid oxygen lr87 lr91-11 iii vacuum
TTTA extracted 43 structured relationships around LR91. Examples in this analysis include LR91 → Application → Upper stage and LR91 → Associated LV → Titan. The table shows each extracted connection, where it came from and its confidence.
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| LR91 | Application | Upper stage | 1.00 | infobox |
| LR91 | Associated LV | Titan | 1.00 | infobox |
| LR91 | Burn time | 247 seconds | 1.00 | infobox |
| LR91 | Chamber | 1 | 1.00 | infobox |
| LR91 | Chamber pressure | 5.93 MPa (860 psi) | 1.00 | infobox |
| LR91 | Country of origin | United States | 1.00 | infobox |
| LR91 | Cycle | Gas-generator | 1.00 | infobox |
| LR91 | Designer | Aerojet | 1.00 | infobox |
| LR91 | Diameter | 1.63 m (5 ft 4 in) | 1.00 | infobox |
| LR91 | Dry mass | 589 kg (1,299 lb) | 1.00 | infobox |
| LR91 | First flight | 1 September 1964 (1964-09-01) | 1.00 | infobox |
| LR91 | Last flight | 19 October 2005 (2005-10-19) | 1.00 | infobox |
| LR91 | Length | 2.81 m (9 ft 3 in) | 1.00 | infobox |
| LR91 | Manufacturer | Aerojet | 1.00 | infobox |
| LR91 | Mixture ratio | 1.86 | 1.00 | infobox |
| LR91 | Nozzle ratio | 49.2 | 1.00 | infobox |
| LR91 | Predecessor | LR91-9 | 1.00 | infobox |
| LR91 | Specific impulse, sea-level | 160 s (1.6 km/s) | 1.00 | infobox |
| LR91 | Specific impulse, vacuum | 316 s (3.10 km/s) | 1.00 | infobox |
| LR91 | Status | Retired | 1.00 | infobox |
| LR91 | Thrust, sea-level | 232.7 kN (52,300 lbf) | 1.00 | infobox |
| LR91 | Thrust, vacuum | 467 kN (105,000 lbf) | 1.00 | infobox |
| LR91 | Thrust-to-weight ratio | 80.85 | 1.00 | infobox |
The concept neighborhoods around LR91 bring nearby vocabulary together. In this analysis, examples include Used, Launch and Liquid. Use the clusters to find adjacent concepts and terminology that may deserve separate research.
For LR91, one of the stronger structural bridges in this analysis connects LR91 with Overview. 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 LR91 to surface related topics, entities, relationships, concept neighborhoods and bridge connections. Use the map to explore areas such as Products, Overview & Versions, including less central topics that may reveal useful research gaps. Automatically extracted connections are research leads rather than rewritten encyclopedia content.
Source: Wikipedia — LR91 · EN edition · Analysis: TopicsToTalkAbout