Embraer Rear Engine turboprop
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Not going to happen here, does it need more wing?
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Originally Posted by ZeroTT
(Post 3279241)
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Might happen. Lot more fuel/carbon efficient.
On typical stages, a modern prop job is almost as fast as a jet. The real drawback was always customer perception. A roomy, quiet turboprop might go over OK, especially if the props in the back somehow alleviate pax innate fear of "crop dusters". I mean it looks high-tech, right? They could lay on the green marketing too. |
Originally Posted by rickair7777
(Post 3279284)
The real drawback was always customer perception. A roomy, quiet turboprop might go over OK.
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I dunno... during a V1 cut, having the props at the rear of the plane are going to create one hell of a yawing moment
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Originally Posted by SonicFlyer
(Post 3279484)
I dunno... during a V1 cut, having the props at the rear of the plane are going to create one hell of a yawing moment
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Originally Posted by ZeroTT
(Post 3279289)
Low wing, loads via jet bridge and has e175 overhead space I think pax will be fine.
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Originally Posted by Hedley
(Post 3279535)
Most passengers are clueless about aviation, however passenger perception would be a significant hurdle. The bigger issue is the size.
and yeah, size is a big issue, although if cost savings are as advertised it could probably be 550’d at a competitive CASM/RASM delta to outgoing crj200/e145 |
Originally Posted by ZeroTT
(Post 3279595)
taking away most of the “this is a turboprop” cues will help a design escape notice of the clueless general public
and yeah, size is a big issue, although if cost savings are as advertised it could probably be 550’d at a competitive CASM/RASM delta to outgoing crj200/e145 |
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