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Second Stage

Assembly

Upper stage with one vacuum-optimised engine and a common-bulkhead tank; it performs the long burn from ~2 km/s staging velocity to orbital insertion. A full specification article for this item is being written. Meanwhile its bill of materials and connections are below.

Bill of materials for Second Stage

4 top-level lines as of r117566
# Item / sub-assembly Part no. Qty/assy Ext. qty Parts Type
1 Vacuum Engine 7 parts orbital-launch-vehicle-vacuum-engine 1× 1 0 assembly
2 Second-Stage Tank 5 parts orbital-launch-vehicle-upper-tank 1× 1 0 assembly
3 Propellant Feed System 6 parts orbital-launch-vehicle-feed-system 1× 1 0 assembly
4 Reaction Control System 3 parts orbital-launch-vehicle-rcs 1× 1 0 assembly