European lunar architecture details leaked

by | Sep 1, 2008 | exploration | 2 comments

Gaetano Marano at his Ghostnasa website has leaked, from a European Space Agency website, an EADS Astruim presentation that was part of a 8 July lunar architecture, industry day

So it would appear that a European Moon mission would require four launches. Two for the lander and its Earth departure stage (EDS) to be sent into orbit around the Moon, probably to dock with an existing lunar station and another two to launch the crew space transportation system and its EDS, which would dock in Earth orbit before going to the Moon.

ESA’s interest in a cislunar space station was already known and the use of such a station as a fuel depot seems to have heavily influenced the European Moonship design with its 16,000kg mass that is substantially less than the NASA Orion crew exploration vehicle’s

So from this it would seem that Astrium is proposing a hypergolic service module engine and probably crew capsule reaction control system. It certainly overcomes the development work that NASA is now undertaking to find a way of storing cryogenic fuels for long durations

The Astrium crew space transportation system design above we have seen before. Even with a refueling depot in low lunar orbit 13,000kg seems a bit low for a final mass to me, assuming that is not dry mass

I do know that today’s Samarra Space Center Soyuz FG can at a push put 16,000kg into LEO, an ESA official told me. But clearly Ariane 5 will need to be upgraded to achieve to 50,000kg and for that the idea is more strap-on solid rocket boosters and a twin Vinci engined upper stage acting as the EDS; an idea ESA’s Bernard Hufenbach told me about a while ago

I am contacting Astrium and ESA and hope to have answers soon

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