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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.
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titan used ii version engine rp-1 stage n2o4 aerozine 50 gas-generator missiles launch ran liquid oxygen lr87 lr91-11 iii vacuum
| 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 | Propellant | .mw-parser-output .template-chem2-su{display:inline-block;font-size:80%;line-height:1;vertical-align:-0.35em}.mw-parser-output .template-chem2-su>span{display:block;text-align:l… | 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 |
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