Thread: Tandem Mi-26?
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Old June 6th 04, 08:55 AM
Tuollaf43
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"Ragnar" wrote in message ...
"Fe" wrote in message
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In article , Ragnar wrote:

"PDR" wrote in message
m...
With all the interest in tactical VTOL and airmobility, has anyone
seriously considered a Chinook type tandem using Mi-26 rotor/engine
combos (or similar scale western versions) at each end?

Should be able to achieve at least 40,000 kg lift over 350-400km. With
a large cabin, medium armour (bradleys, stryker etc.) could be carried
at upwards of 250knots (less retreating tip problems)

Dynamics, stability and control issues should be a lot easier than
with a tiltrotor setup. All in a package maybe 5-8 years to delivery.

And it would be HUGE. Hard to maneuver, needs a bigger LZ than current
designs,


A good deal less than a fixed-wing aircraft, though.


Ever see an Mi-26? Longer fuselage length than a C-130, and the rotors go
108 feet tip to tip.


But have you ever seen Mi-26 lands? Know how much space it needs to
land? Compare that with the landing run required for a hercules
carrying, say a 15ton payload.