(1)
地球表面重力加速度:
g=GM/R^2
=> GM=g R^2
(2)
卫星作匀速圆周运动:
GMm/(R+h)^2=mv^2/(R+h)
=> v=R*sqrt(g/(R+h))
(3)
v=(2pi/T)*(R+h)
=> T=2pi*(R+h)/R* sqrt((R+h)/g)
1、g=GMm/R²,所以GM=gR²/m,
2、F=GMm/(R+h)²=g*R²*m/(R+h)²,
又F=mV²/(R+h)∴V=R*√(g/(R+h))
3、ω=V/(R+h)=R√(g/(R+h)) /(R+h) ,T=2π/ω=2π(R+h)/[R√(g/(R+h))]
√(...)表示里面开方。