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Combustor

Assembly

Annular combustor burning ~3 kg/s of fuel at takeoff with ~1,600 K exit temperature. A full specification article for this item is being written. Meanwhile its bill of materials and connections are below.

Bill of materials for Combustor

2 top-level lines as of r93020
# Item / sub-assembly Part no. Qty/assy Ext. qty Parts Type
1 Combustor Liner jumbo-jet-combustor-liner 1× 1 · part
2 Fuel Nozzle jumbo-jet-fuel-nozzle 20× 20 · part