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Yet another Eve ascent question


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Hi guys,

I'm just wondering how the new atmosphere plays into this ascent.

I did a lot of tests with pre-1.0 using FAR, so it's more a question of whether those findings are still valid. Specifically, do the pointy corners on a lander can (with a nosecone obviously), particularly one with batteries hanging off the side, interfere with drag enough that it's better, or at least comparable, to use a heavier one man command module?

I'm obviously expecting the "probe with a seat" is out the window these days, which I don't so much mind.

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The lander can has a bad aero, the conic command module is a lot better. And no need to go clipped command seat, a good rocket can do the ascent from asl.

I've done landing and reorbiting with a 7 kerbals rocket from 1200m, see sig for report.

Edited by xebx
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