Question

In our search for intelligent life on exoplanets, the feasibility of rocket technology must be considered...

In our search for intelligent life on exoplanets, the feasibility of rocket technology must be
considered on other planets. In order to escape a planets gravity a rocket must attain escape
velocity. If a rocket is to attain this velocity, or at least have enough energy to attain this, then
this can be substituted in for v−v0 in Tsiolkovsky rocket equation. If the exhaust velocity from
the rocket is 4400 m/s, and we assume the maximum amount of propellant practical is 96% (4%
rocket) then estimate the size of a planet where rocket technology is impractical. Assume the
alien planet has the same density of earth. The mass and radius of earth is 5.972×1024 kg and
6.371×106 m, respectively.

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