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Author: WikiMatrix
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English[en]
Another disadvantage is the poor storability of LH2/LOX-powered rockets: Due to the constant hydrogen boil-off, the rocket must be fueled shortly before launch, which makes cryogenic engines unsuitable for ICBMs and other rocket applications with the need for short launch preparations.
Croatian[hr]
Drugi nedostatak je loša sposobnost pohranjivanja LH2 / LOX-pogon raketa: Zbog konstantnog isparavanja vodika, raketa može biti punjena gorivom samo neposredno prije lansiranja, što motore čini neprikladnima za ICBM i druge primjene raketa s potrebom za brzo lansiranje.