It is a rocket engine simulator built using Vuejs and Golang.

The list of inputs to be provided are:

• Specific Heat Ratio
• Combustion chamber temperature
• Mach number
• Combustion chamber pressure
• Exit Pressure
• Expansion Ratio
• Specific Impulse
• Thrust Force
• Nozzle divergence half-angle
• Nozzle convergence half-angle
• Acceleration due to gravity
• Stress on combustion chamber wall

The list of the parameters that are calculated are:

• Exhaust velocity
• Mass flow rate
• Throat area
• Throat radius
• Length of diverging cone
• Area of the inlet at combustion chamber
• Radius of the inlet at combustion chamber
• Length of the converging nozzle
• Length of combustion chamber
• Minimum thickness of combustion chamber wall

• Dynamic visualization of the engine using the values of the parameters entered. (Need help)
• Make the UI better.
• Add more parameters for the engine.

• Clone the repo
• Install packages for Vuejs using npm install.
• Run Vuejs server using npm run serve and Golang server using go run server.go
• Vuejs server will run at http://localhost:8080/ and Golang's at http://localhost:8090/
• Make Changes
• Submit pull request

• Introduction to Rocket Science and Engineering