To get to Mars, use is made of the efficient Hohmann transfer orbit. The spacecraft must first break free from Earth's orbit at 30km / s at a distance of 1UA, then another velocity is added so that its aphelion (152x109m) only approaches the orbit of Mars at 1.52 AU. -Find the length of the semi-major axis if the point where the satellite accelerates is at perihelion (147 x109 m). - what is the period of the satellite? - How long would it take if the aphelion manages to reach Mars? - Why are these missions carried out every 2 years?
To get to Mars, use is made of the efficient Hohmann transfer orbit. The spacecraft must first break free from Earth's orbit at 30km / s at a distance of 1UA, then another velocity is added so that its aphelion (152x109m) only approaches the orbit of Mars at 1.52 AU. -Find the length of the semi-major axis if the point where the satellite accelerates is at perihelion (147 x109 m). - what is the period of the satellite? - How long would it take if the aphelion manages to reach Mars? - Why are these missions carried out every 2 years?
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To get to Mars, use is made of the efficient Hohmann transfer orbit. The spacecraft must first break free from Earth's orbit at 30km / s at a distance of 1UA, then another velocity is added so that its aphelion (152x109m) only approaches the orbit of Mars at 1.52 AU.
-Find the length of the semi-major axis if the point where the satellite accelerates is at perihelion (147 x109 m).
- what is the period of the satellite?
- How long would it take if the aphelion manages to reach Mars?
- Why are these missions carried out every 2 years?
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