In the context of space exploration, what is the primary thermodynamic reason for using cryogenic liquid propellants like liquid hydrogen and liquid oxygen in rocket upper stages?

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Physics · Space Mechanics

In the context of space exploration, what is the primary thermodynamic reason for using cryogenic liquid propellants like liquid hydrogen and liquid oxygen in rocket upper stages?

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They provide a significantly higher specific impulse compared to other chemical propellants.

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They provide a significantly higher specific impulse compared to other chemical propellants.

In the context of space exploration, what is the primary thermodynamic reason for using cryogenic liquid propellants like liquid hydrogen and liquid oxygen in rocket upper stages?

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In the context of space exploration, what is the primary thermodynamic reason for using cryogenic liquid propellants like liquid hydrogen and liquid oxygen in rocket upper stages?

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