S
skywalker01
Guest
Since part of our reason for returning to the Moon is to make use of Lunar materials both for going to Mars and to make manned space exploration affordable and sustainable, I was wondering about past work that has been done on propulsion systems that make use of Lunar materials.<br /><br />Obviously if water ice is available at the Lunar poles in quanity then LOX/LH2 rockets will be possible. But what if it isn't, or if the quanities are too small for a sustained program?<br /><br />There is also a limited body of work that has been done on LOX/Alum rocket motors (Isp approx 267 sec), two materials that were found in quanity at all the Apollo landing sites. But with performance that low is this propellant combination suitable for going to Mars?<br /><br />Then there is the idea of bringing up LH2 or some form of hydrocarbon from Earth and using that in combination with Lunar LOX.<br /><br />But what about some of the higher performance options?<br />Is there a material on the Moon besides LH2 or water in the unproven polar ice that would work with a nuclear thermal rocket or a solar thermal rocket?<br /><br />And is there some propellant combination available on the Moon that could have its performance improved via the addition of thermal, electric, or microwave energy that would make it a better choice than LOX/LH2?<br /><br />And then there is the issue of which idea is most cost effective in terms of both performance, and cost to extract and use. <br />Does anyone know of any work that has been done in this area?<br /><br />Thoughts, ideas, and information welcome.