SUMMARY
This discussion focuses on the construction of an isopropyl alcohol rocket engine, highlighting the challenges of using plastic bottles and the need for a proper combustion chamber. Participants emphasize the importance of calculating the correct ratio of liquid oxygen (LOX) to isopropyl alcohol for optimal thrust production. Additionally, there are warnings against experimenting with LOX without adequate chemical knowledge and suggestions to consider using compressed air as an alternative oxidizer. Safety hazards associated with rocket engine construction are also underscored.
PREREQUISITES
- Understanding of combustion chemistry and stoichiometry
- Knowledge of liquid oxygen (LOX) properties and handling
- Familiarity with rocket engine design principles
- Awareness of safety protocols in experimental rocket propulsion
NEXT STEPS
- Research the optimal LOX to isopropyl alcohol ratio for rocket propulsion
- Learn about the design and function of combustion chambers in rocket engines
- Explore the use of compressed air as an oxidizer in propulsion systems
- Study safety measures and regulations for handling liquid fuels and oxidizers
USEFUL FOR
Aerospace enthusiasts, amateur rocket builders, and individuals interested in propulsion system design and safety protocols in experimental rocketry.