SpaceX launched two GEO comsats, and is about to launch two more, that use all-electric ion propulsion.
Now, I'm wondering, how much time would it take to actually make a satellite like that operational. After all, while ion propulsion is cool and lightweight, it has a very, very low thrust. (Eutelsat 117 West B apparently has only about 200 mN — that's millinewtons — of thrust)
Obviously I can just look it up for an operational satellite, but would be interested in calculating the answer for any arbitrary satellite.
dvmight be off. And of coursemis not constant, but decreasing through the “burn”, so you would have to figure out how much reaction mass is used, then solve a differential equation to get an even-more-accurate value. – Jacob Krall Jun 06 '16 at 12:14