SUMMARY
The energy required to place the space shuttle into orbit at an altitude of 300 km is calculated using gravitational potential energy and kinetic energy equations. The mass of the space shuttle is 6.8 x 104 kg, and the mass of the Earth is 6.0 x 1024 kg. The correct total energy needed is 2.2 x 1012 J, which accounts for the difference between kinetic energy (4.2 x 1012 J) and potential energy (2.1 x 1012 J). The calculations must consider the change in height from the Earth's surface to the orbiting altitude.
PREREQUISITES
- Understanding of gravitational potential energy (GPE) and kinetic energy (KE) equations
- Familiarity with the universal gravitational constant (G = 6.67 x 10-11 N m2/kg2)
- Knowledge of mass and radius of Earth (mass = 6.0 x 1024 kg, radius = 6.4 x 106 m)
- Basic principles of orbital mechanics
NEXT STEPS
- Study the derivation of gravitational potential energy equations
- Learn about the concept of total mechanical energy in orbital motion
- Explore the differences between kinetic and potential energy in space applications
- Investigate the principles of launching spacecraft and achieving orbit
USEFUL FOR
Aerospace engineers, physics students, and anyone interested in the mechanics of space travel and orbital dynamics will benefit from this discussion.