That is a totally different topic. We’re talking about a hypothetical, where Earth is 20-30% larger, not whether an identical copy of Earth but 20-30% larger actually exists nearby. We know such roughly similar exoplanets are common, though. In that size range and in habitable zone.
And again, 30% greater escape velocity just isn’t a challenge. Existing rockets could be used to reach LEO, like Atlas 551 (well, probably want 552 to reduce the gravity losses). And then you can use electric thrusters (which don’t have a hard Isp limit) to reach wherever.
Heck, we could probably reach LEO even if escape velocity was twice what it is. Even 3 times, if you include more exotic propulsion methods that we’ve done some testing for (nuclear thermal, etc). With staging, etc, it’s just a matter of a worse and worse mass fraction, not really whether it’s possible or not. And once you get to low orbit, electric propulsion allows much better scaling as you can adjust Isp higher (although reduces thrust and means it takes longer to do your mission).
And again, 30% greater escape velocity just isn’t a challenge. Existing rockets could be used to reach LEO, like Atlas 551 (well, probably want 552 to reduce the gravity losses). And then you can use electric thrusters (which don’t have a hard Isp limit) to reach wherever.
Heck, we could probably reach LEO even if escape velocity was twice what it is. Even 3 times, if you include more exotic propulsion methods that we’ve done some testing for (nuclear thermal, etc). With staging, etc, it’s just a matter of a worse and worse mass fraction, not really whether it’s possible or not. And once you get to low orbit, electric propulsion allows much better scaling as you can adjust Isp higher (although reduces thrust and means it takes longer to do your mission).