Take-Off Performance
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Join Date: May 2011
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Take-Off Performance
I was looking at some charts (field length vs. still air range) regarding the Avro RJ's take-off performance (but I guess it would also apply to other aircraft) and it looks to me like the take-off length needed has quite a significant impact on range. Is this a correct interpretation of the charts?
If so, I'm assuming that it's because you burn a lot of fuel when you do a steep take off? I guess this makes sense but I wasn't expecting to see such a drastic reduction in range.
Can anyone shed a bit of light on this?
Thanks!
If so, I'm assuming that it's because you burn a lot of fuel when you do a steep take off? I guess this makes sense but I wasn't expecting to see such a drastic reduction in range.
Can anyone shed a bit of light on this?
Thanks!
Join Date: Jan 2003
Location: Southampton
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G'day
I'm no pilot, I be a ATC bloke, but take of run available has a significant impact on range as the shorter the possible run, the lighter the aircraft has to be, so the less payload (pax / freight and FUEL) the aircraft can safely carry. Less fuel, lower range.
F=Ma and all that. If the F of the engines remains the same, the higher the M, the lower the acceleration. Slower acceleration needs more runway to reach the same speed.
Also as the lift created is a function of the speed, to lift a heavier mass you need greater lift and therefore speed. So it's a compounded issue. Higher mass, slower acceleration but a higher speed needed for lift off!
I'm no pilot, I be a ATC bloke, but take of run available has a significant impact on range as the shorter the possible run, the lighter the aircraft has to be, so the less payload (pax / freight and FUEL) the aircraft can safely carry. Less fuel, lower range.
F=Ma and all that. If the F of the engines remains the same, the higher the M, the lower the acceleration. Slower acceleration needs more runway to reach the same speed.
Also as the lift created is a function of the speed, to lift a heavier mass you need greater lift and therefore speed. So it's a compounded issue. Higher mass, slower acceleration but a higher speed needed for lift off!
Join Date: Jun 2004
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Short Runway = Limited Takeoff Weight = Reduced Fuel and/or Payload = Reduced Range.
Nothing to do with "you burn a lot of fuel when you do a steep take off".
Regards,
Old Smokey
Nothing to do with "you burn a lot of fuel when you do a steep take off".
Regards,
Old Smokey