Concept explainers
(a)
The speed of the vehicle as it leaves its circular orbit at A at given condition.
Answer to Problem 13.110P
The required value of the speed is
Explanation of Solution
Given information:
Formula used:
Calculation:
As we have,
And,
We know that:
Put the values in the above equation;
According to conservation of energy;
Put the values in the above equation;
On applying conservation of energy:
According to conservation of angular momentum
Solve for
Put the value of
Conclusion:
The required value of the speed is(b)
The sped at point B at given condition.
Answer to Problem 13.110P
The required value of the speed is
Explanation of Solution
Given information:
Formula used:
Calculation:
We know that,
Put the values in the above equation
Want to see more full solutions like this?
Chapter 13 Solutions
Vector Mechanics For Engineers
- A satellite will travel indefinitely in a circular orbit around the earth if the normal component of its acceleration is equal to g(R/r)2, where g= 9.81 m/s2, R= radius of the earth = 6370 km, and r = distance from the center of the earth to the satellite. Assuming that the orbit of the moon is a circle with a radius of 384 × 103 km, determine the speed of the moon relative to the earth.arrow_forwardAt engine burnout on a mission, a shuttle had reached point A at an altitude of 40 mi above the surface of the earth and had a horizontal velocity v0. Knowing that its first orbit was elliptic and that the shuttle was transferred to a circular orbit as it passed through point B at an altitude of 170 mi, determine (a) the time needed for the shuttle to travel from A to B on its original elliptic orbit, (b) the periodic time of the shuttle on its final circular orbit.arrow_forwardCommunication satellites are placed in a geosynchronous orbit, i.e., in a circular orbit such that they complete one full revolution about the earth in one sidereal day (23.934 h), and thus appear stationary with respect to the ground. Determine (a) the altitude of these satellites above the surface of the earth, (b) the velocity with which they describe their orbit. Give the answers in both SI and U.S. customary units.arrow_forward
- determine (a) the speed of the vehich as it approaches B on the elliptic path, (b) the amount by which its speed should be reduced as it approaches B to insert it into the smaller circular orbit.arrow_forwardA space probe is to be placed in a circular orbit of 5600-mi radius about the planet Venus in a specified plane. As the probe reaches A, the point of its original trajectory closest to Venus, it is inserted in a first elliptic transfer orbit by reducing its speed by ΔvA. This orbit brings it to point B with a much reduced velocity. There the probe is inserted in a second transfer orbit located in the specified plane by changing the direction of its velocity and further reducing its speed by ΔvB. Finally, as the probe reaches point C, it is inserted in the desired circular orbit by reducing its speed by ΔvC. Knowing that the mass of Venus is 0.82 times the mass of the earth, that rA = 9.3 × 103 mi and rB = 190 × 103 mi, and that the probe approaches A on a parabolic trajectory, determine by how much the velocity of the probe should be reduced (a) at A, (b) at B, (c) at C.arrow_forwardThe pilot of an airplane carrying a package of mail to a remote outpost wishes to release the package at the right moment to hit the recovery location A. What angle θ with the horizontal should the pilot’s line of sight to the target make at the instant of release? The airplane is flying horizontally at an altitude of 178 m with a velocity of 239 km/h.arrow_forward
- Determine the speed of a satellite launched parallel to the surface of the earth so that it travels in a circular orbit 800 km from the earth’s surface.arrow_forwardAn expert archer demonstrates his ability by hitting tennis balls thrown by an assistant. A 2-oz tennis ball has a velocity of (32 ft/s)i- (7 ft/s)j and is 33 ft above the ground when it is hit by a 1.2-oz arrow traveling with a velocity of (165 ft/s)j + (230 ft/s)k where j is directed upwards. Determine the position P where the ball and arrow will hit the ground, relative to point O located directly under the point of impact.arrow_forwardThe Clementine spacecraft described an elliptic orbit of minimum altitude hA = 400 km and maximum altitude hB = 2940 km above the surface of the moon. Knowing that the radius of the moon is 1737 km and that the mass of the moon is 0.01230 times the mass of the earth, determine the periodic time of the spacecraft.arrow_forward
- At an amusement park in the greater area there are three 180-kg bumper cars occupied by seniors. The riders in cars A, B, and C have individual masses of 50, 70, and 40 kg respectively. Car A is observed to be moving to the right with a velocity v = 2 m/s and Car C is moving at vc = 1.5 m/s to the left. Car B is initially at rest with a collision imminent. The bumper cars are designed with a coefficient of restitution of 0.8 between each car, VC A B C Determine the final velocity of each car, after all impacts for the following two collision scenarios: (a) Cars A and Chit Car B at the same time, (b) Car A hits Car B before car C does (note there will be more than two total collisions)arrow_forwardTwo spheres A and B, where A has twice the mass of B, are projected at the same horizontal velocity off the edge of two different height shelves. Sphere A leaves from a height of 2.0 m. Sphere B leaves a shelf 1.0 m off the floor. If both spheres leave the edge of the table at the same instant, sphere A will land Im at some time after sphere B. at some time before sphere B. the same time as sphere B. There is not enough information to decide.arrow_forwardA space vehicle is in a circular orbit of 2200-km radius around the moon. To transfer it to a smaller circular orbit of 2080-km radius, the vehicle is first placed on an elliptic path AB by reducing its speed by 26.3 m/s as it passes through A . Knowing that the mass of the moon is 73.49 × 1021 kg, determine (a) the speed of the vehicle as it approaches B on the elliptic path, (b) the amount by which its speed should be reduced as it approaches B to insert it into the smaller circular orbit.arrow_forward
- Elements Of ElectromagneticsMechanical EngineeringISBN:9780190698614Author:Sadiku, Matthew N. O.Publisher:Oxford University PressMechanics of Materials (10th Edition)Mechanical EngineeringISBN:9780134319650Author:Russell C. HibbelerPublisher:PEARSONThermodynamics: An Engineering ApproachMechanical EngineeringISBN:9781259822674Author:Yunus A. Cengel Dr., Michael A. BolesPublisher:McGraw-Hill Education
- Control Systems EngineeringMechanical EngineeringISBN:9781118170519Author:Norman S. NisePublisher:WILEYMechanics of Materials (MindTap Course List)Mechanical EngineeringISBN:9781337093347Author:Barry J. Goodno, James M. GerePublisher:Cengage LearningEngineering Mechanics: StaticsMechanical EngineeringISBN:9781118807330Author:James L. Meriam, L. G. Kraige, J. N. BoltonPublisher:WILEY