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>> No.15704649 [View]
File: 46 KB, 670x425, c3.jpg [View same] [iqdb] [saucenao] [google]
15704649

>>15704633
>If something can do 60 T to TLI is that just saying you can do 60 T to a free-return flyby or something?
I mean, basically. You rarely have the same stage performing both injection and insertion so the mass a rocket can throw at the moon/mars/wherever is more useful for understanding its capability. It's basically what c3 graphs do.

>> No.11552891 [View]
File: 47 KB, 670x425, B6EA2DCD-C49F-4FCE-86A2-7AE61DC590E3.jpg [View same] [iqdb] [saucenao] [google]
11552891

>>11552866
> C3 (km2/s2) from earth to get to various planets : Mars 12, Jupiter 80, Saturn or Uranus 147. To Pluto (with its orbital inclination) needs about 160–164 km2/s2.

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