Ten-engine electric plane completes successful flight test

Eclectic

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NASA is testing a new electric VTOL plane

http://www.sciencedaily.com/releases/2015/05/150505152624.htm

150505152624_1_540x360[1].jpg
 
this was also on their list. this is the latest dragon and the thrusters you see blasting it off the pad are created using 3D printing of the combustion chambers with refractory metal eutectic mixtures not achievable as an alloy.

this technology is so revolutionary that is even more significant than their new battery plant imo.

http://newsdaily.com/2015/05/spacex-puts-dragon-passenger-spaceship-through-test-run/
 
On full scale aircraft you will see twin engine and sometimes quad engine airplanes because it's a major logistical pain in the rear to build a single 2000 horsepower engine, and much easier to build two 1000 horsepower or four 500 horsepower engines.

In the rc world this isn't true because electric motors are built in whatever size you need and generally having more than one motor is just for show because multiple motors means double the losses, and extra weight from the motor housing, escs wires, ect..

I find it interesting that they chose to use so many motors. There must be a benefit of the extra motors that (for lack of a better word) outweighs the penalties of using multiple motors
 
Hillhater said:
Yep, spreading the loads,..
Both physical weight and thrust loads
Means you can have a lighter structure.

Only 4 motors on the Solar Impulse but same concept. Wider than a 747, lighter than many family cars (at 1,600kg):

CGyowhZWQAAVRil.jpg:large
 
parajared said:
On full scale aircraft you will see twin engine and sometimes quad engine airplanes because it's a major logistical pain in the rear to build a single 2000 horsepower engine, and much easier to build two 1000 horsepower or four 500 horsepower engines.

In the rc world this isn't true because electric motors are built in whatever size you need and generally having more than one motor is just for show because multiple motors means double the losses, and extra weight from the motor housing, escs wires, ect..

I find it interesting that they chose to use so many motors. There must be a benefit of the extra motors that (for lack of a better word) outweighs the penalties of using multiple motors


They want to distribute the prop-wash over the entire wing area to have better low vehicle speed wing lift to enable the transition from VTOL to forward flight with less altitude drop during the transition. With enough propwash over your wing, you can make all the lift you need for low speed flight, and do it more efficiently than using thrust alone.
 
Another benefit is redundancy, if the total power is more than you need to stay aloft at whatever your critical altitude/weight is. (cuz then you can afford to lose a prop or motor, and still fly just fine).
 
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