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LE-5B
… It is the first rocket engine in the world which uses the hydrogen used for the cooling of the thrust chamber as the … … Main specifications … Propellant Liquid oxygen/liquid hydrogen Thrust (vacuum) 14 ton Isp (vacuum) 449sec Weight …
https://www.mhi.com/products/space/second_stage_engine_le-5a_le-5b.html
LE-7A
… … Main specifications … Propellant Liquid oxygen/ liquid hydrogen Thrust (vacuum) 112 ton Isp (vacuum) 440sec Weight … … Main specifications … Propellant Liquid oxygen/ liquid hydrogen Thrust (vacuum) 112 ton Isp (vacuum) 440sec Weight …
https://www.mhi.com/products/space/first_stage_engine_le-7_le-7a.html
LE-7A
… … Main specifications … Propellant Liquid oxygen/ liquid hydrogen Thrust (vacuum) 112 ton Isp (vacuum) 440sec Weight …
https://www.mhi.com/group/thacom/products/space/first_stage_engine_le-7_le-7a.html
LE-7A
… … Main specifications … Propellant Liquid oxygen/ liquid hydrogen Thrust (vacuum) 112 ton Isp (vacuum) 440sec Weight …
https://www.mhi.com/group/mhiex/products/space/first_stage_engine_le-7_le-7a.html
MB-XX
… MB-XX 1526 The MB-XX uses liquid oxygen/liquid hydrogen as propellant and is designed as a reliable … … Main specifications … Propellant Liquid Oxygen/ Liquid Hydrogen Thrust (vacuum) 35,000 - 60,000 lbf Isp (vacuum) …
https://www.mhi.com/products/space/space_rocket_engine_mb-xx.html