lpetrich
Contributor
Escape from Proxima b - Scientific American Blog Network -- "A civilization in the habitable zone of a dwarf star like Proxima Centauri might find it hard to get into interstellar space with conventional rockets"
Author Abraham Loeb worked out the numbers, and found it very difficult. Some of his numbers are not the "right" numbers to use, so I'll have to find the correct ones.
First, our Solar System.
The first step in getting off our planet is getting into low Earth orbit. One can go directly into an escape orbit if one can do enough velocity change or delta-V, but low Earth orbit is a minimum for getting into outer space and staying there. For a 300-km altitude, one's orbit velocity is 7.73 km/s and one's orbit period 1.5 hours. One needs about 1 or 2 km/s delta-V more than that to get into orbit, since one must fight our planet's atmosphere and gravity. So one needs 10 km/s delta-V with a high-thrust engine.
Over a century ago, Konstantin Tsiolkovsky worked out from Newtonian mechanics a simple equation that relates rocket initial mass (mi), final mass (mf), exhaust velocity or specific impulse (ve), and the resulting delta-V:
Delta-V = ve * log(mi/mf)
where log is the natural-logarithm function.
Comparison of orbital rocket engines gives the numbers for existing rocket engines. The best high-thrust engines are hydrogen-oxygen ones, and they can have exhaust velocities as 4.5 km/s. Kerosene-oxygen can do 3 km/s, as can UDMH/N2O4 and similar combinations. Solid fuel can do around 2.5 km/s.
This means a mass ratio of 20 - 30 for going into low Earth orbit.
A smaller Earth-composition planet would be easier to travel from, and a larger Earth-composition one harder. From http://astrozeng.com I find these numbers (rock, 30% Fe):
[table="class: grid"]
[tr]
[td]Mass[/td]
[td]Radius[/td]
[td]Surf Grav[/td]
[td]LO Velocity[/td]
[/tr]
[tr]
[td]1.00[/td]
[td]1.005[/td]
[td]0.99[/td]
[td]7.71[/td]
[/tr]
[tr]
[td]2.22[/td]
[td]1.26[/td]
[td]1.41[/td]
[td]10.33[/td]
[/tr]
[tr]
[td]4.29[/td]
[td]1.50[/td]
[td]1.92[/td]
[td]13.19[/td]
[/tr]
[tr]
[td]8.00[/td]
[td]1.75[/td]
[td]2.62[/td]
[td]16.69[/td]
[/tr]
[tr]
[td]13.93[/td]
[td]2.02[/td]
[td]3.42[/td]
[td]20.54[/td]
[/tr]
[/table]
So it would be hard to depart from a super-Earth planet.
The escape velocity is sqrt(2) or 1.414 times the orbit velocity. So one needs 3.22 km/s to escape from low Earth orbit, while for super-Earths, it would also be difficult.
Proxima Centauri b's minimum mass is 1.27 +0.18 -0.17 Earth masses, the minimum figure being reached only for an edge-on orbit. For an orbit tilted with inclination i, one must divide it by sin(i). An inclination of 60d would make it 1.47, 45d 1.80, and 30d 2.54. So that planet is more difficult to depart from than the Earth, but not impossible.
Author Abraham Loeb worked out the numbers, and found it very difficult. Some of his numbers are not the "right" numbers to use, so I'll have to find the correct ones.
First, our Solar System.
The first step in getting off our planet is getting into low Earth orbit. One can go directly into an escape orbit if one can do enough velocity change or delta-V, but low Earth orbit is a minimum for getting into outer space and staying there. For a 300-km altitude, one's orbit velocity is 7.73 km/s and one's orbit period 1.5 hours. One needs about 1 or 2 km/s delta-V more than that to get into orbit, since one must fight our planet's atmosphere and gravity. So one needs 10 km/s delta-V with a high-thrust engine.
Over a century ago, Konstantin Tsiolkovsky worked out from Newtonian mechanics a simple equation that relates rocket initial mass (mi), final mass (mf), exhaust velocity or specific impulse (ve), and the resulting delta-V:
Delta-V = ve * log(mi/mf)
where log is the natural-logarithm function.
Comparison of orbital rocket engines gives the numbers for existing rocket engines. The best high-thrust engines are hydrogen-oxygen ones, and they can have exhaust velocities as 4.5 km/s. Kerosene-oxygen can do 3 km/s, as can UDMH/N2O4 and similar combinations. Solid fuel can do around 2.5 km/s.
This means a mass ratio of 20 - 30 for going into low Earth orbit.
A smaller Earth-composition planet would be easier to travel from, and a larger Earth-composition one harder. From http://astrozeng.com I find these numbers (rock, 30% Fe):
[table="class: grid"]
[tr]
[td]Mass[/td]
[td]Radius[/td]
[td]Surf Grav[/td]
[td]LO Velocity[/td]
[/tr]
[tr]
[td]1.00[/td]
[td]1.005[/td]
[td]0.99[/td]
[td]7.71[/td]
[/tr]
[tr]
[td]2.22[/td]
[td]1.26[/td]
[td]1.41[/td]
[td]10.33[/td]
[/tr]
[tr]
[td]4.29[/td]
[td]1.50[/td]
[td]1.92[/td]
[td]13.19[/td]
[/tr]
[tr]
[td]8.00[/td]
[td]1.75[/td]
[td]2.62[/td]
[td]16.69[/td]
[/tr]
[tr]
[td]13.93[/td]
[td]2.02[/td]
[td]3.42[/td]
[td]20.54[/td]
[/tr]
[/table]
So it would be hard to depart from a super-Earth planet.
The escape velocity is sqrt(2) or 1.414 times the orbit velocity. So one needs 3.22 km/s to escape from low Earth orbit, while for super-Earths, it would also be difficult.
Proxima Centauri b's minimum mass is 1.27 +0.18 -0.17 Earth masses, the minimum figure being reached only for an edge-on orbit. For an orbit tilted with inclination i, one must divide it by sin(i). An inclination of 60d would make it 1.47, 45d 1.80, and 30d 2.54. So that planet is more difficult to depart from than the Earth, but not impossible.