Respuesta :
Answer:
7.78 * 10³ m/s
Explanation:
Orbital velocity is given as:
v = √(GM/R)
G = 6.67 * 10^(-11) Nm/kg²
M = 5.98 * 10^(24) kg
R = radius of earth + distance of the satellite from the surface of the earth
R = 2.15 * 10^(5) + 6.38 * 10^(6)
R = 6.595 * 10^(6) m
v = √([6.67 * 10^(-11) * 5.98 * 10^(24)] / 6.595 * 10^(6))
v = √(6.048 * 10^7)
v = 7.78 * 10³ m/s
The speed of the satellite at the given radius is 7,776.9 m/s.
The given parameters;
- mass of the satellite, m = 500 kg
- distance of the satellite, r = 215 km
- radius of the earth, r' = 6,380,000 m
- mass of earth, M = 5.98 x 10²⁴ kg
The speed of the satellite is calculated as follows;
[tex]F = \frac{GMm}{R^2} = \frac{mv^2}{R} \\\\v^2 = \frac{GM}{R} \\\\v = \sqrt{\frac{GM}{R}}[/tex]
where;
- R is the distance between the center of the earth and the satellite
R = 215,000 m + 6,3800,000 m
R = 6,595,000 m
[tex]v = \sqrt{\frac{GM}{R}}\\\\v = \sqrt{\frac{6.67\times 10^{-11} \times 5.98 \times 10^{24} }{6,595,000}}\\\\v = 7,776.9 \ m/s[/tex]
Thus, the speed of the satellite at the given radius is 7,776.9 m/s.
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