Models

Domain model layer representing the physical components of a rocket propulsion system. This is where you define your motor, propellant, grain geometry, thrust chamber, and feed system.

Submodules:

• motors — SolidMotor and LiquidEngine definitions
• propellants — Propellant components, formulations, and thermochemical properties
• grain — Grain geometry and burn regression models
• thrust_chamber — Nozzle, combustion chamber, and injector
• feed_systems — Feed system models for liquid engines

machwave.models