PPRuNe Forums - View Single Post - Multiple rotor vs single rotor efficiency
Old 18th December 2007 | 21:19
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slowrotor
 
Joined: Jul 2003
Posts: 440
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From: Port Townsend,WA. USA
Thanks Nick,
I am trying to design an airplane with powered lift to allow flight at a lower speed only for takeoff and landing. The powered lift would only be used about 5 seconds or so. The efficiency is not important in this case I contend.

This is a lesson I learned when you were discussing the lack of efficiency of the Harrier jump jet. I think a Harrier test pilot said the Harrier only used about 100 lbs of fuel to make a landing. Sure the Harrier is not efficient in hover but that is not the mission. I also watched a C-130 equipped with 8 JATO rockets take off in a short distance and climb briefly very steep. JATO is not efficient for long haul but probably more efficient for just the needed 15 second thrust.

I think the future of personal VTOL aircraft is more likely to be fixed wing with brief powered lift. It's a different mission than a working helicopter that must hover for long periods.
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