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Most frustrating were difficulties with the ramjet engine, which was necessary for sustained supersonic flight.
The ramjet engine would not be on the rail, but part of the vehicle itself.
His group invented the propulsion system for Talos, the first surface-to-air missile to use a ramjet engine.
Effects of gas temperature, gas pressure, oxygen mole fraction on boron ignition and combustion in ramjet engine were studied and could be useful for ramjet engine design.
An implementable nonlinear control design approach is presented for a supersonic air-breathing ramjet engine.
ATREX is a fan-boosted ramjet engine using liquid hydrogen as a fuel and coolant.
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The performance of combined-cycle PDTEs is compared with baseline afterburning turbofan and ramjet engines.
The turbojet, pulse-jet, and ramjet engines, on the other hand, carry only their fuel and depend on the oxygen content of the air for burning.
Ramjet engines have significant advantages when compared to conventional rocket motors concerning specific impulse, manoeuvrability, and range.
In the flight Mach number range considered, from 4 to 7, the overall efficiency of both the supersonic-combustion and the conventional ramjet engines increases with flight speed.
The gains obtained are outstanding for both the combined-cycle PDTE modes compared to baseline turbofan and ramjet engines.
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