Will fly late next year? Where have I heard that one before...
Will fly late next year? Where have I heard that one before...
A line like that sets off some big flashing red lights for me. Either they're incompetent and have grossly underestimated the amount of work needed to complete this, or it's a scam.
The real issue that I'm not seeing addressed is capital. No investors listed anywhere.
[1] http://www.bloomberg.com/news/articles/2016-03-21/this-aeros...
EDIT: Forgot to actually include the link.
Their webpage has a bunch of guys standing around what looks like a Vietnam-era jet engine.
Also, if they're planning to have something flying in 20 months, they should be beyond the cardboard and plywood mockup phase of development.
The more I see about this company the more I think it's a scam.
For comparison, the Concorde took about 21 years to develop. Granted, it was a massive clusterfuck, but they also had to solve a lot of issues along the way.
Sure they can. It's the inlet's job to slow the flow to subsonic. Turbofans have been used on supersonic military aircraft since the 1960's. Go read about intake ramps. Then learn about diverterless supersonic intakes.
You're yelling scam pretty loud for someone that clearly doesn't know basics of the topic area.
Edit: My guess is the engine they're standing in front of is a JT8 of some flavor, which have been heavily used by both military and commercial aircraft.
There are several 4th generation fighters with sustained supersonic cruise, as well as older aircraft like the B1. The basic technology has been around for decades. Nothing about the proposed supersonic small commuter jet is impossible from an engineering perspective, though aspects of it won't be _easy_, and it is entirely possible the business case doesn't work out.
I mostly replied above because of the categorical statement that supersonic flight with turbofans is impossible. The reality is that virtually all supersonic aircraft use engines with some bypass. The Concorde's engines oddly enough are one of the few zero bypass designs used in industry.
The problem is that when you get closer to 1:1 scale, new always issues come up with bigger challenges. You solve one problem at 1:5 scale, only to realize that doesn't work at 1:3 and the whole thing needs to be redesigned from the ground up.
The annals of aviation history are littered with aircraft unable to move past 1:n scale.
Didn't Burt Rutan make a composite aircraft from design to first flight in a year back in the 80s?
Getting the aircraft certified and into production is where most of the actual expense is.