Liquid-propellant rocket
Rocket, Rocket engine, Propellant, Liquid, Mass ratio
978-613-5-83603-5
613583603X
112
2011-08-01
39.00 €
eng
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Please note that the content of this book primarily consists of articles available from Wikipedia or other free sources online. A liquid-propellant rocket or a liquid rocket is a rocket with an engine that uses propellants in liquid form. Liquids are desirable because their reasonably high density allows the volume of the propellant tanks to be relatively low, and it is possible to use lightweight pumps to pump the propellant from the tanks into the engines, which means that the propellants can be kept under low pressure. This permits the use of low mass propellant tanks, permitting a high mass ratio for the rocket.
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