SUMMARY
The altitude of satellite S, which travels at a constant speed of 20 Mm/h (5555.6 m/s) with a centripetal acceleration of 2.5 m/s², is calculated using the formula for centripetal acceleration, a_n = v²/ρ. By rearranging this equation, the radius ρ is determined to be approximately 12,345,679.01 m. Subtracting the Earth's radius (6,356,500 m) from this value yields an altitude of approximately 5,989.18 km. The initial confusion arose from incorrectly using the Earth's diameter instead of its radius in the calculations.
PREREQUISITES
- Understanding of centripetal acceleration and its formula a_n = v²/ρ
- Knowledge of unit conversions, specifically from Mm/h to m/s
- Familiarity with the Earth's dimensions, including its radius and diameter
- Basic algebra skills for rearranging equations and performing calculations
NEXT STEPS
- Study the principles of circular motion and centripetal acceleration in physics
- Learn about unit conversions and their importance in scientific calculations
- Explore the implications of altitude on satellite operations and orbital mechanics
- Investigate the effects of gravitational forces on satellite trajectories
USEFUL FOR
Students in physics or engineering, satellite engineers, and anyone involved in orbital mechanics or satellite design will benefit from this discussion.