please make it obvious what the answer and units are. thanks!
please make it obvious what the answer and units are. thanks! INTER VERSION BACK NET RCES...
Chapter 05, Problem 31 GO Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 448 km above the earth's surface, while that for satellite B is at a height of 926 km. Find the orbital speed for (a) satellite A and (b) satellite (a) VA- (b) V- Show Work is REQUIRED for this questions Open Show Work
Chapter 05, Problem 31 GO Your answer is partially correct. Try again. Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 361 km above the earth's surface, while that for satellite B is at a height of 780 km. And the orbital speed for (a) satellite A and (b) satelite (a) VA (1) Ve Click If you would like to Show Work for this questioni Modi Show Work
Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 364 km above the earth's surface, while that for satellite B is at a height of 880. km. Find the orbital speed for satellite A and satellite B. (a) VA = (b) VB =
Need some help answering this question. Please show all work and use appropriate units. Thanks. s. billionaire puts a satellite into orbit The Moon orbits the Earth once every 27.3 days. Suppose that a crazy around the Earth, so that the satellite etes ctly 5 orbits of the during every 3 orbits of the Moon. compl Earth (Assume that both orbits are circular.) a. (3 pts. Calculate the ratio of the orbital radi of the satellite and the Earth's Moon....
numbers, the other with the equations. Put a box around the answer to each part. 1. An object's circular orbital velocity vc around the earth can be calculated using the equation ", where ve is the circular orbital velocity, μ-3.98601 E5 km3/s, is the earth's gravitational parameter, and r is the distance of the object from the earth's center. Some commercial satellites, like DirecTV, are in an orbit where they take one sidereal day (23h 56m 4.09s) to orbit the...
please make answer and units clear! thanks MESSAGE HY INSTRUCTOR FULL SCREEN PRINTER VERSION BACK Chapter 05, Problem 38 GO A satellite has a mass of 5926 kg and is in a circular orbit 4.43 x 10 m above the surface of a planet. The period of the orbitis 1.hours. The radius of the planet is 4.73 x 10 m. What would be the true weight of the satelliteit were at rest on the planet's surface? w the tolerance is...
Newton's version of Kepler's Law Force Example Use what we know about the earth's orbit to estimate the mass of the sun. For this problem we can use Newton's form of Kepler's law Solving for the sum of the masses we get to use this law we need all our values to be kilograms, meters, and seconds. a 1AU-149.6x10P m and p- 1 year (365.25 days/year)(24 hours/day)(3600 seconds/hour)-3.15x 10" sec. Placing these values in to our equation we get M+...
please help me answer this question PHY Homework. • Equations are in a separate document entitled "Equations for Rotational Dynamics Assignment" • Moments of inertia formulas are provided on the last page of this document • Show all of your work when solving equations. It is not sufficient to merely have a correct numerical answer. You need to have used legitimate equations and algebra. You also need to have correctly used the data. • Units must be specified for any...