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RL10

Boeingin Delta IV-kantoraketin toisen rakettivaiheen RL-10B-2-rakettimoottori

RL-10 on 1960-luvulla kehitetty yhdysvaltalainen rakettimoottori, joka ensimmäisenä maailmassa käytti polttoaineenaan nestevetyä ja hapettimena nestehappea.


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