Thrust Chamber Assembly
AssemblyRegeneratively cooled combustion chamber and bell nozzle where propellants burn at ~10 MPa and accelerate to supersonic exhaust. A full specification article for this item is being written. Meanwhile its bill of materials and connections are below.
Bill of materials for Thrust Chamber Assembly
6 top-level lines as of r98971| # | Item / sub-assembly | Part no. | Qty/assy | Ext. qty | Parts | Type |
|---|---|---|---|---|---|---|
| 1 | Injector Head 5 parts | liquid-rocket-engine-injector | 1× | 1 | 0 | assembly |
| 2 | Chamber Liner | liquid-rocket-engine-chamber-liner | 1× | 1 | · | part |
| 3 | Chamber Jacket | liquid-rocket-engine-chamber-jacket | 1× | 1 | · | part |
| 4 | Nozzle Extension | liquid-rocket-engine-nozzle-extension | 1× | 1 | · | part |
| 5 | Coolant Manifold | liquid-rocket-engine-coolant-manifold | 2× | 2 | · | part |
| 6 | Acoustic Cavity Ring | liquid-rocket-engine-acoustic-cavity | 1× | 1 | · | part |