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Scientists want to place a 4200 kg satellite in orbit around Mars. They plan to have the satellite orbit at a speed of 2484 m5) What should the speed of the orbit be, if we want the satellite to take 8 times longer to complete one full revolution of

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Answer #1

Given is:-

Mass of the satellite m_s = 4200 kg

Orbital speed of the satellite  v = 2484 m/s

mass of the mars  m_m = 6.4191 \times 10^{23}kg

radius of the mars  r_m = 3.397 \times 10^6 m

Now,

part - 1

The radius of the orbit is given by

\frac{m_sv^2}{r} = \frac{Gm_sm_m}{r^2}

by plugging all the values we get

\frac{(4200 kg)(2484 m/s)^2}{r} = \frac{(6.67 \times 10^{-11}N-m^2/kg^2 )(4200 kg)(6.4191 \times 10^{23}kg)}{r^2}

which gives us

\boxed{r = 6.94 \times 10^6 m}

Part -2 the force of attraction between the mars and the satellite is given by

F = \frac{(6.67 \times 10^{-11}N-m^2/kg^2 )(4200 kg)(6.4191 \times 10^{23}kg)}{(6.94 \times 10^6m)^2}

which gives us

\boxed{F = 3733.62 N}

Part - 3

The acceleration of the satellite is given by

a = \frac{F}{m}

thus

a = \frac{3733.62N}{4200kg}

which gives us

\boxed{a =0.89 m/s^2}

Part - 4

as we know that

\frac{m_s v^2}{r} = \frac{Gm_sm_m}{r^2}

or

r = \frac{Gm_m}{v^2}

hence,

the radius of the orbit would depend on

\\\boxed{ \text{ mass of the planet}} \\ \boxed{\text{ speed of the satellite}}

Part - 5

Time to take one revolution

T = \frac{2 \pi r}{v}

Now if we want the satelitte to take 8 time longer time, then

T' = 8 T

thus

8 ( \frac{2 \pi r}{v}) = \frac{2 \pi r}{v'}

which gives us

v' = \frac{v}{8}

by plugging the values of velcoity v of satellite we get

v' = \frac{2484 m/s}{8}

which gives us

\boxed{v' =310.5 m/s}

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