Further, both the fuel and oxidizer have high boiling points compared to other rocket fuels (such as liquid hydrogen) and oxidizers (such as liquid oxygen), allowing rockets to be stored ready for launch for long periods without the fuel or oxidizer boiling off and needing to be replenished.
Furthermore, the fuel and oxidizer exhibit elevated boiling points compared to other rocket propellants (like liquid hydrogen) and oxidizers (like liquid oxygen). This characteristic permits rockets to be kept in a state of readiness for launch over prolonged periods without the fuel or oxidizer evaporating and requiring replenishment.