Announcement
75 kN kerolox rocket engine presented as a Noyron-generated reference design
Leap 71 says the open-cycle engine design is suitable for the first stage of a microlauncher or the upper stage of a larger orbital vehicle.
TLDR
Leap 71 shared a Noyron-generated reference design for a 75 kN (16,900 lbf) open-cycle kerolox rocket engine. The company says its combustion chamber and injector are designed for additive manufacturing in CuCrZr, a high-temperature copper alloy. It uses reference engines in different configurations to test Noyron’s models.
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