K
krrr
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Most of you will be aware of the lunar flyby proposal by Energia which is promoted by Space Adventures (for 100M $ per "tourist" passenger).<br /><br />Basically, a Soyuz spacecraft would dock with a Zenit-launched Block-DM stage, which would then hurl the Soyuz into a free-return lunar flyby trajectory.<br /><br />As noted on astronautix.com, the Block-DM would barely be able to provide the necessary delta-v for trans lunar insertion (TLI), which is about 3150 m/s. So maybe the Soyuz' own propulsion would have to supply an additional kick (the Soyuz has a delta-v capability of 390 m/s).<br /><br />Anyway, I think a lunar <font color="orange">flyby</font>is not very cool. I wouldn't pay 100 million dollars for that.<br /><br />Lunar <font color="orange">orbit</font>is a different thing.<br /><br />There are different types of lunar orbits: a low lunar orbit (say a circular 100 km orbit) requires more than 800 m/s delta-v for braking into it (lunar orbit insertion, LOI), and a similar amount of delta-v to escape from it (trans-earth insertion, TEI).<br /><br />What I envision is a <font color="orange">highly elliptical lunar orbit</font>(HELO): For instance, a 12-hour orbit with a perilune of 100 km and an apolune of 8700 km. This requires only 300 m/s for LOI and less for TEI. Passengers (and scientific instruments) would have a close look at the Moon twice a day.<br /><br />Let's look at the payload capabilities of current (non-US) launchers:<br /><br />TLI:<br />Zenit+DM: 4 tonnes<br />Proton+DM: 4.5 tonnes<br />Proton+Breeze: 5.8 tonnes<br />Ariane 5 ECA: /> 7 tonnes<br />Proton+KVRB: ~ 8 tonnes<br /><br />EOR+TLI:<br />Zenit+DM: < 7 tonnes<br />Proton+DM: ~ 8 tonnes<br />Proton+Breeze: ~10 tonnes<br />Pro