For certain space-based experiments a satellite must provide its occupants with an…

PHYSICS · Multi-part · A Level · Physics · Fields and their consequences · Fields and their consequences

Problem

For certain space-based experiments a satellite must provide its occupants with an effective downward acceleration of only 3.0 m s−23.0\,\text{m\,s}^{-2} while they remain in a circular orbit around the Earth. (a) Calculate the orbital radius (measured from the Earth’s centre) at which the centripetal acceleration of the satellite equals 3.0 m s−23.0\,\text{m\,s}^{-2}. Use ME=5.97×1024 kgM_{\rm E}=5.97\times10^{24}\,\text{kg} and G=6.67×10−11 N m2 ⁣/kg2G=6.67\times10^{-11}\,\text{N\,m}^2\!\text{/kg}^2. (b) Hence find the altitude of this orbit above the Earth’s surface (RE=6.37×106 mR_{\rm E}=6.37\times10^{6}\,\text{m}). (c) For an astronaut of mass 70 kg70\,\text{kg} inside the satellite, calculate the gravitational force acting on the astronaut at that altitude and express it as a percentage of the astronaut’s weight at the Earth’s surface.

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