Editing Pumped Gas Rocket Engine
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== Description == <!--T:2--> | == Description == <!--T:2--> | ||
The pumped gas rocket engine uses a 2:1 mix of [[Volatiles]] to [[Oxygen]]. It has a maximum thrust of 16.2kN and contributes 500kg to the overall weight of the rocket. | The pumped gas rocket engine uses a 2:1 mix of [[Volatiles]] to [[Oxygen]]. It has a maximum thrust of 16.2kN and contributes 500kg to the overall weight of the rocket. | ||
β | To travel to mars orbit it is recommended the rocket weigh less than | + | To travel to mars orbit it is recommended the rocket weigh less than 8000kg. |