Determine if there is sufficient cooling by radiation to prevent the combustion chamber/nozzle from becoming too hot.

Part V. and Part vii Discuss your propellant tanks here. Include a discussion of material, size, shape, etc. You will also need to determine the type of propellant feed system. You will need to calculate the thrust-to-initial weight ratio. For pressure fed systems and blowdown systems, you need to determine the mass of feed gas […]