SUMMARY
The energy required to boost the Space Shuttle from a 250 km orbit to a 610 km orbit is calculated to be 1.17 x 1011 J. This calculation incorporates both potential and kinetic energy, utilizing the gravitational constant G = 6.67 x 10-11 N(m/kg)2 and the mass of the Earth Me = 5.98 x 1024 kg. The initial potential energy at the lower orbit (Ug1) is -4.519 x 1012 J, while the potential energy at the higher orbit (Ug2) is -4.286 x 1012 J, leading to a change in mechanical energy (∆Emech) of 1.17 x 1011 J.
PREREQUISITES
- Understanding of gravitational potential energy and kinetic energy equations
- Familiarity with the gravitational constant (G = 6.67 x 10-11 N(m/kg)2)
- Knowledge of mass and radius in orbital mechanics
- Ability to perform calculations involving large numbers and scientific notation
NEXT STEPS
- Study the derivation of gravitational potential energy equations in orbital mechanics
- Learn about the principles of energy conservation in space travel
- Explore the effects of altitude on orbital velocity and energy requirements
- Investigate the mechanics of the Space Shuttle and its propulsion systems
USEFUL FOR
Aerospace engineers, physics students, and anyone involved in space mission planning or orbital mechanics will benefit from this discussion.