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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/N 2 O 4. [1] This engine was vacuum optimized and ran the gas-generator cycle. The thrust chamber used fuel for regenerative cooling, with separate ablative skirt. [1]
The Solar T62 Titan is an American gas turbine engine used mainly as a aircraft auxiliary power unit (APU), conventional power generator, turboprop engine for fixed-wing aircraft or turboshaft engine for helicopters.
Used on the Titan I, the LR87-3 burned liquid oxygen and RP-1. [4] Following the retirement of the Titan missile program, these engines saw no further use. [citation needed] The LR87-3 was also operated with NTO/Aerozine 50 and ground tested with LOX/H2 (with a new fuel pump), making it one of very few engines to have been run on three different propellant combinations.
Titan 350 Titan 250 Titan 130 Mars 100 ... pump-drive packages and generator sets. ... International Harvester placed Solar Division's radial engine designs into the ...
Engine Origin Designer Vehicle Use Propellant ... Gas generator 302.3–313 8,580–20,470 ... Titan IV: Booster: PBAN: Solid fuel 272 [100] 245 (SL) 7,116,000
They used 2 ft-4 main propulsion engines, 2 ft-12 cruise engines and 3 Solar Saturn 750 kW generators. An LM2500 gas turbine on USS Ford The first U.S. gas-turbine powered ship was the U.S. Coast Guard's Point Thatcher , a cutter commissioned in 1961 that was powered by two 750 kW (1,000 shp) turbines utilizing controllable-pitch propellers. [ 92 ]
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