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Talk:Exploration Systems Architecture Study

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This is an old revision of this page, as edited by Subzero788 (talk | contribs) at 06:13, 31 January 2006. The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

Lunar Mission Profile

The article reads: "The EDS will brake the complex into lunar orbit". I believe that, according to the selected profile, lunar orbit insertion is performed by the CEV instead. Balix 00:29, 3 January 2006 (UTC)[reply]

Actually I believe the descent engine of the LSAM (lunar surface access module) will facilitate lunar orbit insertion. Subzero788 06:13, 31 January 2006 (UTC)[reply]