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Why do you say the inclination is different? You can go into LEO at any inclination. I also don't see why you need more delta-v to go from launch orbit to circ
by lutorm 16y ago
Why do you say the inclination is different? You can go into LEO at any inclination.
I also don't see why you need more delta-v to go from launch orbit to circular orbit to transfer orbit compared to the transfer orbit directly. My orbital mechanics are rusty, but it seems to me that since you need to lift the perigee from Earth's surface to Mars orbit, you'll pass the circular orbit on the way.
- bfe 16y agoIf you go into low Earth orbit from the Earth's surface, you need to go into an orbital inclination equal to the latitude of your launch site - which is extremely unhelpful if you want to then take that mass anywhere else in the solar system. You also need to circularize your orbit, then later boost that mass from circular orbit to hyperbolic escape orbit - also extremely wasteful.
- lutorm 16y agoOk, good point about the inclination. I still don't see why circularizing the orbit would be wasteful. Circularizing an elliptical orbit at apogee still requires positive delta-v, which will help you on the way to the hyperbolic orbit. Only if you want to circularize at perigee would you need to slow down, which would indeed be extremely wasteful. It's true that you get more energy boost for the delta-v if you do it early rather than late, but I don't know if the ellipticity of the launch orbit is high enough for that difference to qualify as "extremely" wasteful. But maybe it is.