Calculating Satellite Speed and Orbit Height
Introduction
- Calculating the speed of a satellite in a circular orbit.
- Understanding centripetal and gravitational forces.
- Deriving equations to find speed, period, and height.
Satellite Speed Calculation
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Centripetal Force: Provided by gravity.
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Gravitational Force Equation:
[ F = \frac{G \cdot M \cdot m}{R^2} ]
- (G): Universal gravitation constant.
- (M): Mass of Earth.
- (m): Mass of the satellite.
- (R): Distance between Earth's and satellite's centers.
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Centripetal Force Equation:
[ F = \frac{m \cdot v^2}{R} ]
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Speed Calculation: Derived Equation:
[ v = \sqrt{\frac{G \cdot M}{R}} ]
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Distance (R):
- Earth's radius: (6.38 \times 10^6) meters.
- Satellite height: 3800 km = (3.8 \times 10^6) meters.
- (R = 1.018 \times 10^7) meters.
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Calculate Speed:
- Plug values into the speed equation.
- Result: (6254.3) m/s.
Calculating the Period of the Satellite
Geosynchronous Satellite
- Geosynchronous Period: Same as Earth's rotation period.
- One rotation: 24 hours.
- Convert to seconds: (86,400) seconds.
Satellite Height Calculation
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Relation between Period and Radius:
- Derived from speed and gravitational equations.
- [ R^3 = \frac{G \cdot M \cdot T^2}{4\pi^2} ]
- [ R = \sqrt[3]{\frac{G \cdot M \cdot T^2}{4\pi^2}} ]
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Calculate Orbital Radius (R):
- Result: (4.22 \times 10^7) meters.
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Calculate Satellite Height (H):
[ H = R - \text{Earth's Radius} ]
- Result: (3.58 \times 10^7) meters or 35,800 km.
Calculate Satellite Speed in Geosynchronous Orbit
- Speed Calculation using Orbital Radius:
- Formula: [ v = \sqrt{\frac{G \cdot M}{R}} ]
- Result: 3072 m/s.
Summary
- Calculated speed, period, and height for satellites in circular and geosynchronous orbits.
- Utilized gravitational dynamics and orbital mechanics.
This comprehensive summary covers how to determine the speed, period, and height of a satellite using equations derived from gravitational and centripetal forces. The explanation includes how these principles apply to both general satellites and geosynchronous satellites.