Question

Consider a satellite at an altitude of 700 km above Earth, with its velocity perpendicular to...

Consider a satellite at an altitude of 700 km above Earth, with its velocity perpendicular to the direction to Earth. If the satellite would have a velocity that is 0.2 km/s larger than the local escape velocity, what would the excess velocity V∞ be?

The answer was 2.07 km/s.

I would like to know the detailed steps to reach that answer

Homework Answers

Answer #2

answered by: anonymous
Know the answer?
Your Answer:

Post as a guest

Your Name:

What's your source?

Earn Coins

Coins can be redeemed for fabulous gifts.

Not the answer you're looking for?
Ask your own homework help question
Similar Questions
An Earth satellite has a semi-latus rectum (p) altitude of 7400 km. When the satellite is...
An Earth satellite has a semi-latus rectum (p) altitude of 7400 km. When the satellite is at its semi-latus rectum, it has a velocity of 6.5 km/s. Find the orbit's semi major axis.
A satellite is in circular orbit at an altitude of 1800 km above the surface of...
A satellite is in circular orbit at an altitude of 1800 km above the surface of a nonrotating planet with an orbital speed of 3.7 km/s. The minimum speed needed to escape from the surface of the planet is 8.4 km/s, and G = 6.67 × 10-11 N · m2/kg2. The orbital period of the satellite is closest to 59 min. 83 min. 75 min. 67 min. 51 min.
A satellite is in circular orbit at an altitude of 1500 km above the surface of...
A satellite is in circular orbit at an altitude of 1500 km above the surface of a nonrotating planet with an orbital speed of 3.4 km/s. The minimum speed needed to escape from the surface of the planet is 8 km/s, and G = 6.67 × 10-11 N · m2/kg2. The orbital period of the satellite is closest to A)59 min. B)45 min. C)72 min. D)65 min. E)52 min.
A satellite orbits the Earth uniformly in a circular orbit with a velocity of magnitude 4.00...
A satellite orbits the Earth uniformly in a circular orbit with a velocity of magnitude 4.00 km/s. Use Newton's gravitation force as the force in Newton's Law of Acceleration, using also the centripetal acceleration . Solve for radius r of the satellite's orbit in terms of v . (a) Find then the altitude of the satellite above the surface of the Earth. Earth's mass and radius are 5.9810 kg and 6.3810 km. (b) Find the time it takes the satellite...
The satellite is rotating round the Earth at 500 km above the ground. The mass of...
The satellite is rotating round the Earth at 500 km above the ground. The mass of the Earth is B) 6 × 10^24 kg, the radius of the Earth is 6400 km. Gravitational constant -11 3 -1 -2 G=6.67408 × 10 m kg s . A) What is the velocity of the satellite? If the mass of the satellite is m=1000kg, how much work should be done to move it to the higher orbit 1000 km above the Earth?
A satellite of mass 180 kg is placed into Earth orbit at a height of 700 km above the surface....
A satellite of mass 180 kg is placed into Earth orbit at a height of 700 km above the surface. (a) Assuming a circular orbit, how long does the satellite take to complete one orbit?  h (b) What is the satellite's speed?  m/s (c) Starting from the satellite on the Earth's surface, what is the minimum energy input necessary to place this satellite in orbit? Ignore air resistance but include the effect of the planet's daily rotation.
A satellite 595 km above the earth's surface transmits sinusoidal electromagnetic waves of frequency 92.6 MHz...
A satellite 595 km above the earth's surface transmits sinusoidal electromagnetic waves of frequency 92.6 MHz uniformly in all directions, with a power of 25.0 kW. A- What is the intensity of these waves as they reach a receiver at the surface of the earth directly below the satellite? B- What is the amplitude of the electric field at the receiver? C- What is the amplitude of the magnetic field at the receiver? D- If the receiver has a totally...
1. An Earth satellite moves in a circular orbit 615 km above the Earth's surface. The...
1. An Earth satellite moves in a circular orbit 615 km above the Earth's surface. The period of the motion is 96.8 min. (a) What is the speed of the satellite? (b) What is the magnitude of the centripetal acceleration of the satellite? 2. A rotating fan completes 1200 revolutions every minute. Consider a point on the tip of a blade, at a radius of 0.17 m. (a) Through what distance does the point move in one revolution? (b) What...
i) Explain the difference between a man-made and a natural satellite. ii) State two important advantages...
i) Explain the difference between a man-made and a natural satellite. ii) State two important advantages of weather satellites. iii) Starlink is a satellite constellation being constructed by SpaceX to provide global satellite Internet access. The constellation will consist of thousands of small satellites in low earth orbit. A Starlink launch to an altitude of 550km is required. The Falcon 9 launcher delivers 9.0 metric tonnes payload into a LEO orbit. The lift-off mass is 318 tonnes. The U of...
Consider a 200 kg spacecraft orbiting the Earth. The vehicle’s position at a given time (lets...
Consider a 200 kg spacecraft orbiting the Earth. The vehicle’s position at a given time (lets call it time zero), relative to a non-rotating reference frame with origin at Earth’s centre, is r = −5310i + 5040j km. Its velocity vector at time zero is v = −4.85i − 6.37j km/s. 1. Calculate the distance from Earth’s centre to the spacecraft, the speed of the spacecraft, and the specific angular momentum (magnitude and direction) relative to Earth’s centre at time...
ADVERTISEMENT
Need Online Homework Help?

Get Answers For Free
Most questions answered within 1 hours.

Ask a Question
ADVERTISEMENT