SUMMARY
The forum discussion centers on the design of a lunar-capable spacecraft intended to carry 8-10 crew members and two landers or cargo. The user is in the early design phase, grappling with fitting a LOx/LH2 fuel system into a 15 by 30 ft space. Key insights include the importance of defining mission requirements, the challenges of launching from Earth's surface, and the need for a feasible design that considers aerodynamic demands and fuel consumption. Participants emphasize starting with smaller-scale prototypes and gaining practical experience before attempting a full-scale model.
PREREQUISITES
- Understanding of LOx/LH2 fuel systems
- Knowledge of spacecraft design principles
- Familiarity with aerodynamic testing methods
- Basic concepts of rocket propulsion and launch systems
NEXT STEPS
- Research the design and specifications of the Space Shuttle and SLS (Space Launch System)
- Learn about the principles of aerodynamic testing for spacecraft
- Investigate model rocket design and construction techniques
- Explore the fuel consumption statistics and performance metrics of Space Shuttle Main Engines (SSMEs)
USEFUL FOR
Aerospace engineering students, hobbyist rocket enthusiasts, and individuals interested in spacecraft design and development.