diesel engine microlight pendulum

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Christophe
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View Christophe » 21/02/12, 09:18

From what I understand, it can pass in 2 (depending on the mass limit) :)

Me too the ULM model would interest me well (I have just passed the theoretical at the DGAC ... mention instructor sivouplé! 8) ) ...

These are only self-built for the moment, is there a possibility of buying "ready-made" (used?)? And at what cost?
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antoinet111
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View antoinet111 » 21/02/12, 10:08

both, the plans are the same.
however, no opportunities, people don't sell them.

but many parts are made.
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Macro
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View Macro » 21/02/12, 10:32

antoinet111 wrote:both, the plans are the same.
however, no opportunities, people don't sell them.

but many parts are made.


And what makes the difference between the two? transportable weight ???
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View Christophe » 21/02/12, 10:42

No big difference: the airplane version is probably between 500 and 600 kg ...

But by plane, you can imagine a 4-seater version not with a larger cell ...

But with the same dimensions (except cell), the wing loading would be much higher ... therefore higher stall speed. Same for load factor when cornering ...

We should continue this debate in the subject dedicated to the gazail: https://www.econologie.com/forums/moteurs-di ... t2250.html
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antoinet111
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View antoinet111 » 21/02/12, 11:55

just the wing area in this case.

far enough in construction you may not have made your choice between ULM and airplane.
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