地球同步卫星加速度a1、线速度v1.半径r1.
近地卫星加速度a2、线速度v2.半径r2.
地球半径R.
根号:√ 3次根:|3√
a=GM/r^2=v^2/r=4π^2/T^2xr
r1=|3√[GMT^2/(4π^2)] r2=R
a1=4π^2/T^2x|3√[GMT^2/(4π^2)] a2=GM/R^2
a1 :a2=4π^2/T^2x|3√[GMT^2/(4π^2)] :GM/R^2
v1=√{GM/ |3√[GMT^2/(4π^2)] } v2=√(GM/R)
v1 :v2=√{GM/ |3√[GMT^2/(4π^2)] } :√(GM/R)
答:a1 :a2=4π^2/T^2x|3√[GMT^2/(4π^2)] :GM/R^2.v1 :v2=√{GM/ |3√[GMT^2/(4π^2)] } :√(GM/R).