Hasil (
Bahasa Indonesia) 1:
[Salinan]Disalin!
1-6 ROCKET ENGINESNon-air-breathing propulsion systems are characterized by the fact that they carry both fuel and the oxidizer within the aerospace vehicle. Such systems thus may be used anywhere in essential features of a liquid-propellant rocket system. Two propellants (an oxidizer and a fuel) are pumped into the combustion to chamber where they ignite. The nozzle accelerates the products of combustion to high velocities and exhausts them to the atmosphere or space.
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