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The kinetic energy of an object is energy due to its motion and its mass. Here's the formula: Ek = 1/2 mv2 Kinetic energy is equal to one half times the mass of the object times the square of its velocity. You can see that the velocity factor has a bit more importance because velocity is squared to calculate kinetic energy. To discover the kinetic energy of a satellite, you'll need to know its mass and its orbital speed. Orbital speed will vary depending on the height of the orbit, and its eccentricity. In circular orbits, speed can be constant, and it may range from just under 7 km/sec to just under 8 km/sec. In eliptical orbit, the figures can vary even more ('cause it moves faster when its at perigee - closer to earth, and slower when it's at apogee - farthest away). If you want actual numbers, you'll have to supply the mass of the orbiting body and specify an orbital path. Naturally you've got links to related Wikipedia articles to help you, and those links are below.
What else can I help you with?
What would be the effect on the orbital velocity of satellite if mass of satellite is double?
Doubling the mass of a satellite would result in no change in its orbital velocity. This is because the orbital velocity of a satellite only depends on the mass of the planet it is orbiting and the radius of its orbit, but not on the satellite's own mass.
Is the satellite accelerating?
Yes, the satellite is accelerating because it is revolving around our earth and in a circular motion so its velocity changes every second so it is accelerating.A2. No, the satellite is not accelerating. Acceleration is defined as the rate of change of velocity. But, its velocity is constant. The centrifugal effect is exactly balanced by the pull of gravity (assuming a circular orbit).But a nice question. The net acceleration between these forces is zero.
What is the shape of the orbit when the velocity of the satellite is everywhere perpendicular to the force of gravity?
If the velocity of the satellite is always perpendicular to the force of gravity, then the eccentricity of the orbit is zero, and it's perfectly circular.
If a satellite's radial velocity is zero at all times its orbit must be elliptical or parabolic?
Not necessarily. A circular orbit around a central body, such as a planet, would also have a radial velocity of zero at all times. In a circular orbit, the satellite's velocity vector is always perpendicular to the radius vector, resulting in a constant radial velocity of zero.
Is the critical velocity equal to orbital velocity of satellite?
Balance of force of gravity by centripetal forceYes, for any given orbital radius (r) only one velocity will give stable orbit, this is called the critical velocity.Pick your orbital radius and satellite mass (m)Use Gmm / r2 to calculate gravitational force (f),then find velocity from : v = sq root ( (r * f ) / m)
What would be the effect on the orbital velocity of satellite if mass of satellite is double?
Doubling the mass of a satellite would result in no change in its orbital velocity. This is because the orbital velocity of a satellite only depends on the mass of the planet it is orbiting and the radius of its orbit, but not on the satellite's own mass.
The tangential velocity of an Earth satellite is its velocity?
The tangential velocity of an Earth satellite is its velocity perpendicular to the radius vector pointing towards the center of the Earth. It represents the speed at which the satellite is moving along its orbital path. This velocity is crucial for maintaining the satellite's orbit and is calculated using the satellite's distance from the center of the Earth and gravitational force acting upon it.
What is the method for determining the angle of projection in projectile motion?
The angle of projection in projectile motion is determined by using the formula: arctan(vy / vx), where is the angle of projection, vy is the vertical component of the initial velocity, and vx is the horizontal component of the initial velocity.
Calculations of critical velocity of satellite?
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What does perturbation do to a satellite?
it affect the path and orbital velocity of satellite due to gravitation pull
The velocity required to keed a satellite in orbit around the Earth is called?
circular velocity
What is the effect of this force on velocity of the satellite?
The force acting on a satellite will cause a change in its velocity according to Newton's second law, which states that force equals mass times acceleration (F=ma). If the force is in the same direction as the velocity, it will cause the satellite to speed up; if it is in the opposite direction, it will cause the satellite to slow down.
If you keep th velocity of projection and change the angle of projection from 75 degrees to 45 degrees what will happen to the horizontal distance the projectile travels?
If you keep th velocity of projection and change the angle of projection from 75 degrees to 45 degrees what will happen to the horizontal distance the projectile travels? if you finish the nova net lesson you might learn the answer! It will travel a greater distance!
The force of gravity is responsible for continuously changing the what of a satellite?
The force of gravity is responsible for continuously changing the velocity or speed of a satellite as it orbits around a larger body, such as a planet or a star. This change in velocity helps to maintain the satellite's orbit and keep it in motion around the larger body.
If you keep the velocity of projection constant and change the angle of projection from 75 to 45 what will happen to the horizontal distance the projectile travels?
The horizontal distance will be doubled.
Is the satellite accelerating?
Yes, the satellite is accelerating because it is revolving around our earth and in a circular motion so its velocity changes every second so it is accelerating.A2. No, the satellite is not accelerating. Acceleration is defined as the rate of change of velocity. But, its velocity is constant. The centrifugal effect is exactly balanced by the pull of gravity (assuming a circular orbit).But a nice question. The net acceleration between these forces is zero.
How do sattalites get up in to space?
escape velocity of satellite is greater
