SUMMARY
The Apollo Command Module (CM) utilized helium tanks primarily for the reaction control subsystem, which was essential for propellant feed during attitude control. This system was crucial for maneuvering the spacecraft, especially during re-entry after the Service Module was jettisoned. The discussion highlights the importance of helium in maintaining stability and control of the CM throughout its mission phases.
PREREQUISITES
- Understanding of spacecraft systems and subsystems
- Knowledge of propulsion and attitude control mechanisms
- Familiarity with the Apollo program and its components
- Basic principles of gas storage and utilization in aerospace applications
NEXT STEPS
- Research the Apollo Command Module's reaction control subsystem
- Study the role of helium in spacecraft propulsion systems
- Explore the design and function of the Apollo Service Module
- Learn about attitude control thrusters used in re-entry scenarios
USEFUL FOR
Aerospace engineers, space historians, students of aerospace technology, and anyone interested in the operational mechanics of the Apollo program.