For smaller, low performance rockets such as attitude control thrusters where high performance is less necessary, a pressurised fluid is used as propellant that simply escapes the spacecraft through a propelling nozzle.
22.
Propelling nozzles may have a fixed geometry, or they may have variable geometry to give different exit areas to control the operation of the engine when equipped with an afterburner or a reheat system.
23.
Current low-bypass military turbofans include the Pratt & Whitney F119, the Eurojet EJ200, the General Electric F110, the Klimov RD-33, and the Saturn AL-31, all of which feature a mixed exhaust, afterburner and variable area propelling nozzle.
24.
The airflow through the intake was being induced, or pumped, by the gas generator and heated with maximum afterburner, which gave a thrust distribution, at Mach 3 +, of 54 % inlet, 17.6 % engine, 28.4 % propelling nozzle.
25.
The exhaust gas temperature ( EGT ) of the thermoreactor using the Humphrey cycle being lower than in the conventional Brayton cycle by hundreds of degrees, the exhaust airflow out of the propelling nozzles at the trailing edge of the front wings can be directed onto the upper surface of the rear wings.
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