Suppose the space shuttle is in orbit 500 km from the Earth's surface, and circles the...

Question

Question

Suppose the space shuttle is in orbit 500 km from the Earth's surface, and circles the Earth about once every 90 min .

a) Find the centripetal acceleration of the space shuttle in its orbit.

b) Express your answer in terms of g, the gravitational acceleration at the Earth's surface.

Answer 1

Answer #1

Here

h=500 km

the Earth about once every T=90 min

Answer 2

Similar Homework Help Questions

The space shuttle typically travels in a circular orbit at an altitude of 500 km above...

The space shuttle typically travels in a circular orbit at an altitude of 500 km above the Earth's surface. The Earth itself has a radius of about 6400 km. The shuttle can travel in a circular orbit, at constant speed, without any need for the rocket engine to be on, if it travels at just the right speed (a) Given that the value of g is 8.50 m/s2 at an altitude of 500 km, determine the value of the shuttle's...
A satellite is in a 91.0 min period circular orbit 330 km above Earth's surface. A)Find...

A satellite is in a 91.0 min period circular orbit 330 km above Earth's surface. A)Find the satellite's speed. B)Find its centripetal acceleration.
An Earth satellite moves in a circular orbit 724 km above Earth's surface with a period...

An Earth satellite moves in a circular orbit 724 km above Earth's surface with a period of 99.07 min. What are (a) the speed and (b) the magnitude of the centripetal acceleration of the satellite? 3 sig figs please

2. Support the space shuttle is in orbit about the earth at 400 km above its...

2. Support the space shuttle is in orbit about the earth at 400 km above its surface. Determine the orbital speed and the orbital period of the space shuttle. 3.calculate the minimum velocity (escape speed) a spacecraft must have to escape the gravitational force of the planet earth. Mearth=5.972 x 10^24kg 4. Calculate the schwarzschild radius of a black hole with the mass of the sun.Mearth=5.972 x 10^24kg
The International Space Station typically travels in a circular orbit at an altitude of 400 km...

The International Space Station typically travels in a circular orbit at an altitude of 400 km above the Earth's surface. The Earth itself has a radius of about 6400 km. Assume that the space station travels in a circular orbit at constant speed (this is a perfectly reasonable assumption). A. Given that the value of g is 8.68m/s28.68m/s2at an altitude of 400 km, determine the value of the space station's speed in its circular orbit. _______ m/s B. At this...
What is the orbital period for a circular orbit at 2100 km above the Earth's surface?...

What is the orbital period for a circular orbit at 2100 km above the Earth's surface? You may assume that the mass of the Earth is about 5.97x1024 kg and that the radius of the Earth is about 6371 km. 129 min O 128 min 125 min 138 min 131 min

An Earth satellite moves in a circular orbit 808 km above Earth's surface with a period...

An Earth satellite moves in a circular orbit 808 km above Earth's surface with a period of 100.8 min. What are (a) the speed and (b) the magnitude of the centripetal accelerat ion of the satellite? (a) Number747E3 Units m b) Numberi7.7 Units m/s 2
Chapter 04, Problem 056 An Earth satellite moves in a circular orbit 775 km above Earth's...

Chapter 04, Problem 056 An Earth satellite moves in a circular orbit 775 km above Earth's surface with a period of 100.1 min. What are (a) the speed and (b) the magnitude of the centripetal acceleration of the satellite? (a) Number Units (b) Number Units
Problem 3) The space shuttle is in a circular orbit of 180 km altitude and inclination 30o. What ...

Problem 3) The space shuttle is in a circular orbit of 180 km altitude and inclination 30o. What is the change in east longitude (AX) of the ascending node after 1 orbit of the satellite? (answer in radians) Hint: ёл-(w Earth-A)nT for n orbits Problem 3) The space shuttle is in a circular orbit of 180 km altitude and inclination 30o. What is the change in east longitude (AX) of the ascending node after 1 orbit of the satellite? (answer...

Imagine yourself in geostationary orbit, this is in an orbit that circles the earth every 24...

Imagine yourself in geostationary orbit, this is in an orbit that circles the earth every 24 hours. That is about 6 and a half earth radii out from the center of the earth. Now imagine tether running from geostationary orbit to 1000 km closer to the earth and 1000 km further from the center of the earth. Would a person at either end of the tether feel like they are in zero g, or would they feel a small acceleration...