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Liquid Apogee Engine

Assembly

Bipropellant rocket engine firing at apogee to circularize the orbit at GEO. A full specification article for this item is being written. Meanwhile its bill of materials and connections are below.

Bill of materials for Liquid Apogee Engine

2 top-level lines as of r34389
# Item / sub-assembly Part no. Qty/assy Ext. qty Parts Type
1 Thrust Chamber & Nozzle communications-satellite-thrust-chamber 1× 1 · part
2 Propellant Valve 2 parts communications-satellite-prop-valve 2× 2 0 assembly