/

Solar-powered space flight

3e. Power required to reach earth orbit ignoring atmospheric drag: Corresponding figures for various other bodies in the solar system

[this page | pdf | references | back links]

Return to Abstract and Contents

Next page

 

3.11        The Earth is the largest of the inner planets and therefore the most challenging in terms of the required  to reach orbit. Even though Mars is circa 1.524 times as far away from the sun as the Earth, its smaller size and therefore lower surface gravity and orbital velocity more than compensate for the smaller amount of solar power available per unit area in its vicinity, see Figure 5. The same also appears to be true for all but the largest moons of Jupiter and Saturn even though they are considerably further away from the sun.

 

Figure 5. Values of  (for different propellant to lifted mass ratios), assuming vehicle travels horizontally and with propellant ejected at optimal speeds (subject to an upper limit of 10,000 ms-1) and optimal angles, for the Earth, Moon and Mars

 


NAVIGATION LINKS
Contents | Prev | Next


Desktop view | Switch to Mobile