The fact is I am the only person who has provided any documentation regarding the workings of the deflectors.
Providing the documentation is one thing. Understanding it is another.
I find it comical on how everyone has twisted this MIT paper to mean nothing.
Please show us where we have 'twisted' the memo rather than pointing out some pretty significant caveats.
And once again, do you understand the difference between a paper and a memo? This is not trivial.
And to suggest that these conclusions have no bearing to the LM flying solo (detached from the CSM). If anything, it is even more problematic for the LM operating solo.
The graph in that memo specifically contradicts that assertion.
Atleast the CSM-LM had the ability of disabling the LM RCS’s if there is a failure or mismatch power issue ( ie one RCS operating at 50 percent of the opposite RCS) and rely on the CSM RCS’s.
No, the stacked vehicle only ever used the RCS on the service module in normal flight. It did not have to 'disable' the LM RCS because they were only intended to be used when the LM was flying solo.
(That is what happen with Apollo 13, I have the report)
If you have the report how are you making such a fundamental error in fact? On Apollo 13 the CSM was shut down and the LM RCS used to control attitude when required. This is the only time the LM RCS was used to control the stacked vehicle, and it wasn't done by automatic control.
But with the LM operating alone there is no backup if there is a failure or mismatch of power between two opposite thrusters and that will result in serious stability issues.
No, it won't, for reasons already explained.