| ▲ | phire 2 hours ago | |||||||||||||
Is a Mach-5 passenger aircraft actually the goal of this project? Seems more likely that Japan is designing this engine for a hypersonic cruise missile program, and the passenger aircraft concept is somewhat of a cover. IMO, there is no point in a Mach-5 Aircraft (other than cruise missiles). There is potentially some point in Mach 2-3 aircraft, (not that we have ever made them commercially viable) but at the boundary to hypersonic, you might as well just switch to a suborbital hop concept. A suborbital hop gets you to anywhere in the world within ~90min, avoids issues of supersonic overflight and you don't need to worry about the massive engineering issues caused by sustaining hypersonic flight. And as a bonus, the passengers get a hour of weightlessness. | ||||||||||||||
| ▲ | numpad0 29 minutes ago | parent | next [-] | |||||||||||||
Air breathing engines don't need the oxidizer tank, so like the 2/3 of a rocket just goes away before even touching Tsiolkovsky math. That improves payload mass fraction massively. Also, this doesn't scale down to Mach 3-4 and under. This thing uses scramjet, or supersonic combustion ramjet. It REQUIRES intake air to be at high supersonic speeds for it to work. | ||||||||||||||
| ▲ | adev_ an hour ago | parent | prev | next [-] | |||||||||||||
> you might as well just switch to a suborbital hop concept. One is not exclusive to the other. Skylon was expected to use air breathing engine up to Mach5+ and switch to rocket engine beyond it. You can probably do the same for a suborbital airliner if you are insane enough. | ||||||||||||||
| ▲ | m4rtink 2 hours ago | parent | prev [-] | |||||||||||||
90 minutes is a full low Earth orbit cycle. For a suborbital hop it should be about half of that at maximum for any 2 points on Earth. | ||||||||||||||
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