NASSP
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LM Systems Implementation Phase 1
LM systems implementation for Apollo 9/10 features. Hardware used or tested in Apollo 9/10 should be able to perform the functions tested during those missions.
#603
Most LM systems have been implemented, is there anything else major that is missing other than a few heaters or changes that would be involved in a major EPS or PROP rework?
Doubling back to this, I think the LM can handle 9 and 10 fully flown currently, only exceptions are specific spacecraft panels and AGS software plus flight test software flown on 9.
I'd say this can be closed at this point