Space/Science — HabitableZone

Space/Science » in reply to You wrote: "You'll find that the detonation velocity for hydrogen-air at STP is 1968 m/sec"

re: The only design for a scramjet that works in theory

has combustion take place for a short time (perhaps 10 seconds, I forget), and then coasting for at least as long, allowing convection to cool the engine, before restarting. I read the published description of the hypersonic propulsion system in the SAE Aerospace Journal, and it included magnetron ionization of the airflow to allow instant combustion of hydrogen and oxygen. I tossed the journal in the blue box several years ago. They published too often, if I didn't throw them out they'd have created a fire hazard!

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