Если вдруг кому-то интересно, то Crew Dragon contains approximately 2562.79 kg of hypergolic propellant, including approximately 1587.57 kg of nitrogen tetroxide (NTO) and 975.22 kg of monomethylhydrazine (MMH).
(Source: Draft Environmental Assessment for Issuing SpaceX a Launch License for an In-flight Dragon Abort Test, Kennedy Space Center, Brevard County, Fl. - FAA, NASA and USAF, Nov 2018)