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Data: G-6.67 x 10 Nm /kg Rearth 6378 km; me-5.97 x 104 kg m.-2.88 x 104 kg (for CSM module) height of orbit-185 km a) Find th

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Answer #1

a] F = GMeMs/(REarth +height)^2

= 6.67e-11*5.97e24*2.88e4/(6378000+185000)^2

= 266249 N

b] Gravitational PE = -GMeMs/(REarth +height)

= -6.67e-11*5.97e24*2.88e4/(6378000+185000)

= -1.747*10^12 J

c]   Gravitational force = centripetal force

GMeMs/r^2 = Ms*v^2/r where v = sqrt(GMe/r)

  GMe/r = v^2

v = sqrt(GMe/r) where r = REarth +height

= sqrt(6.67e-11*5.97e24/(6378000+185000))

= 7789 m/s = 7789*2.237 mph = 17424 mph answer

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