An artificial satellite moving in a circular orbit around the earth has a total (kinetic + potential) energy E0 Its potential energy is [IIT 1997 Cancelled; MH CET 2002; MP PMT 2000]
A rocket of mass M is launched vertically from the surface of the earth with an initial speed V. Assuming the radius of the earth to be R and negligible air resistance, the maximum height attained by the rocket above the surface of the earth is [AMU 1995]
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Two bodies of masses m1and m2 are initially at rest at infinite distance apart. They are then allowed to move towards each other under mutual gravitational attraction. Their relative velocity of approach at a separation distance r between them is [BHU 1994; RPET 1999]
A projectile is projected with velocity kve in vertically upward direction from the ground into the space. (ve is escape velocity and k<1 If air resistance is considered to be negligible then the maximum height from the centre of earth to which it can go, will be : (R = radius of earth) [Roorkee 1999; RPET 1999]
A satellite is launched into a circular orbit of radius R around the earth. A second satellite is launched into an orbit of radius (1.01)R. The period of the second satellite is larger than that of the first one by approximately [IIT 1995]
If the distance between the earth and the sun becomes half its present value, the number of days in a year would have been [IIT 1996; RPET 1996]
A geostationary satellite orbits around the earth in a circular orbit of radius 36000 km. Then, the time period of a satellite orbiting a few hundred kilometres above the earth?s surface (R(Earth)=6400km) will approximately be [IIT-JEE (Screening) 2002]
If an artificial satellite is moving in a circular orbit around the earth with a speed equal to half the magnitude of the escape velocity from the earth, the height of the satellite above the surface of the earth is:
.The time period of a simple pendulum at the centre of earth is
.A satellite is orbiting very close to planet. Its time period depends only upon: