: The earth moves round the sun in à circular orbit of radius 1.5 × 108 km. Calculate B. E. of the earth. Mass of sun = 2 × 1030 kg, radius of earth = 6400 km, g = 9.8 m/s² %3D
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![: The earth moves round the sun in a
circular orbit of radius 1.5 × 108 km. Calculate
B. E. of the earth. Mass of sun = 2 × 100 kg,
radius of earth = 6400 km, g = 9.8 m/s²
%3D
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- A rocket, launched from the Earth, shuts off its engines when its speed is 5.10 km/s. It reaches a maximum altitude of 2600 km before it falls back to Earth. At what altitude did the rocket's engines shut off? The mass and radius of the Earth are 5.97 1024 kg and 6.37 106 m, respectively. kmAn artificial satellite circles the Earth in a circular orbit at a location where the acceleration due to gravity is 5.42 m/s. Determine the orbital period of the satellite. min Need Help? Read ItA uniform distribution of dust in the solar system adds to the gravitational attraction of the Sun on a planet an additional forceF = −m C rwhere m is the mass of the planet, C is a constant proportional to the gravitational constant and the density of the dust, and r is the radius vector from the Sun to the planet (both considered as points). This additional force is very small compared to the direct Sun-planet gravitational force.Calculate the period for a circular orbit of radius r0 of the planet in thiscombined field.
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- Suppose that humans have created a colony outside of our solar system on a planet called Cheops5. Cheops5 has a mass of 2.25×10^25 kg and a day that lasts 29.9 h (which defines the rotational period of the planet). The colony is located on the planet's equator. The colonists set up a communications satellite which orbits Cheops5. The satellite has a circular orbit that keeps it positioned directly above the colony. Calculate the radius ?r of the satellite's orbit in kilometers.4. We are planning a human exploration mission to Mars. We will first place our spacecraft into a circular around Mars and then send down a lander. a) If we want the spacecraft to orbit at an altitude of 170 km above the Martian surface, what will the velocity and orbital period of the spacecraft? b) When we land astronauts on the surface of Mars, what acceleration due to gravity in terms of g's (i.e. as a fraction of the Earth's gravitational acceleration) will the astronauts experience? You are permitted to use an online resource (e.g. Google) to find the necessary information about Mars that you might need in solving this problem.