Physics, asked by anul5, 1 year ago

A spaceship is stationed on Mars. How much energy must be expended on the spaceship to launch it out of the solar system? Mass of the space ship = 1000 kg; mass of the Sun = 2 × 1030 kg; mass of mars = 6.4 × 1023 kg; radius of mars = 3395 km; radius of the orbit of mars = 2.28 × 108kg; G= 6.67 × 10–11 m2kg–2.​

Answers

Answered by jack6778
1

Answer:

Mass of the spaceship, ms = 1000 kg

Mass of the Sun, M = 2 × 1030 kg

Mass of Mars, mm = 6.4 × 10 23 kg

Orbital radius of Mars, R = 2.28 × 108 kg =2.28 × 1011m

Radius of Mars, r = 3395 km = 3.395 × 106 m

Universal gravitational constant, G = 6.67 × 10–11 m2kg–2

Potential energy of the spaceship due to the gravitational attraction of the Sun = -GMms / R

Potential energy of the spaceship due to the gravitational attraction of Mars = -GMmms / r

Since the spaceship is stationed on Mars, its velocity and hence, its kinetic energy will be zero.

Total energy of the spaceship = -GMms / R - GMmms / r

= -Gms[ (M / R) + (mm / r) ]

The negative sign indicates that the system is in bound state.

Energy required for launching the spaceship out of the solar system

= – (Total energy of the spaceship)

= Gms[ (M / R) + (mm / r) ]

= 6.67 × 10-11 × 103 × [ (2 × 1030 / 2.28 × 1011) + (6.4 × 1023 /3.395 × 106 ) ]

= 596.97 × 109 = 6 × 1011 J.

Answered by Anonymous
3

Answer:

Explanation:

PE of spaceship due to sun = -GMm(s) / R 

PE of spaceship die to Mars = -GM(m) m(s)/r

KE = 0 

Total Enrgy = -GMm(s) + Gm(s) M(m) /r

= -GM(s)[ M/R + M(m) / r] 

Energy = Gm(s) [M/R + M(m) /r]

= 6.67 x 10^-11 x 10^3 [ 2 x 10^30 / 2.28 x 10^11 + 6.4 x 10^23 / 3.395 x 10^6]

= 6.67 x 10^-8 x 89.56 x 10^17

= 596.6 x 10^9 

= 6.0 x 10^11 J (aprox) 

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