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....And now for a slight thread-hijack:
OK, so no one here is arguing against the end-product: An electrically-powered propeller or ducted fan. Can I stop for a minute and say "WTF?" to the recent article about how jet engines are the future of self-launch? (I think this was in SOARING magazine, IIRC) Jets are wonderful devices for specific missions (especially sustained thrust at higher speeds, where props become less efficient). But in a glider, at low speed and for short periods of time? The article talks about how the jets are improving and becoming more and more suited to use in a sailplane... But: 1) You still have to carry a dangerous, liquid, flammable fuel. Oh, and that fuel can turn to vapor that might incapacitate the pilot if breathed, and the fuel can EAT your aircraft's core materials in some cases, if it seeps into the structure - yipes! 2) Despite being reliable and simple compared to an internal- combustion engine, jet engines still have as much or more complexity than a simple electric motor. The heat and stress on bearings and other parts has got to be higher than an electric motor, right? 3) Jets put out a LOT more HEAT than an electric motor. Can anyone tell me how resins that cure at ambient-temperature levels are supposed to hold up well when a jet engine retracts inside the fuselage while its still hot? I've heard that they can cool down efficiently in as little as 30 - 45 seconds; but what about operator error? What about the distance / altitude lost during that wait period? I know the drag of a turbine is less than a big ol' prop; but still... 4) With a jet, you already need electrical equipment, for the starters and igniters and such. Why add a whole second fuel/energy-delivery system (i.e. Jet-A) when you can stick with a single source and a single output? OK, OK, I'll quit ranting... :-P --Noel |
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