地球半径为R,表面的重力加速度为g,一颗人造卫星在距地面高2R处做匀速圆周运动,求此卫星的线速度,周期和向心加速度
人气:149 ℃ 时间:2019-11-04 09:09:14
解答
F=mv^2 / r = G*Me*m / r^2
v = √(GMe/r)
v=wr w=v/r= √(GMe/r) / r
T = 2π/v = 2π/√(GMe/r)
a= GMe / (2r)^2= 1/4g
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