What propellants are they using? They talk frequently about "cryogenics," so I can probably guess that the oxidizer is LOX, but I can't rule out a semi-cryogenic kerolox engine, and nowadays both methalox and hydrolox are possibilities for "full" cryogenic.
(Excluding more exotic things like Isar's propane/LOX, but barring further evidence I'm assuming they're going with one of kerolox, methalox, or hydrolox.)
Interesting. Does the use of ethanol and peroxide for the test engines tell us anything about what they're likely to use for the real thing? My gut says "probably not hydrogen, since that's so unique that ethanol just can't replicate it," but my only training in rocket science is "I read Ignition! once."