Rocket Propulsion Analysis
RPA is a multi-platform analysis tool for conceptual and preliminary design of chemical rocket engines capable of:
- Engine performance analysis
- Thrust chamber sizing
- Nozzle wall contour optimization
- Thrust chamber cooling analysis
- Engine cycle power balance analysis
- Engine mass estimation
- Scripting utility for development of custom solutions
Engine definition
Hihg-level parameters of the engine.
Nozzle flow model specification
Estimated chamber performance
Thermodynamic properties of gas at different chamber stations
Estimated chamber performance
Ideal and estimated delivered performance
Thrust chamber size and geometry
Design parameters
Thrust chamber size and geometry
Estimated thrust chamber size and geometry
Propellant feed system
Design parameters
Propellant feed system
Estimated operating parameters
