Classification -- Definitions and fundamentals -- Nozzle theory and thermodynamic relations -- Flight performance -- Chemical rocket propellant performance analysis -- Liquid propellant rocket engine ...
Fundamentals of thermodynamics and aerodynamics -- Thermodynamic cycle analysis of gas turbines and air-breathing propulsion systems -- Aerodynamic design of axial flow compressors and turbines -- ...
Essentially, a nuclear rocket engine is a reactor that has hydrogen running through it as a propellant, which is heated to an astonishing 3,000 K (2,727 °C, 4,940 °F), giving it almost twice the ...
XCOR Aerospace announced today that it had won a $3.3 million contract with ATK as part of ATK’s contract to develop low-cost LOX/methane rocket propulsion for NASA. Together with ATK, XCOR will ...
Critical to one of the world’s largest solar array assemblies, the solar panels will enable NASA’s Gateway lunar space station to be the most powerful electric propulsion spacecraft ever flown.
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