We had a meeting on April 9 which was extremely interesting to me. We discussed and settled on how the MSFN tracking and sextant landmark observations would be used in the MCC/RTCC to produce optimum DOI and Descent targeting for the LM. The big new factor that had to be taken into account somehow was…
Category: F
F/G Mission Techniques – except for the lunar orbit phase – are ready to eat
Some of the decisions and open items that came out of our F/G Mission Techniques meetings in late January are listed in this memo. Basically, I would say that all mission phases aside from the lunar orbit activity are very well understood at this time – primarily as a result of the C’ mission -…
F Rendezvous Mission Techniques
We had our first F Rendezvous Mission Techniques meeting on November 12. We went through the whole thing rather smoothly with very few open items, probably due to all the past work on D and G. Obviously it is a much simpler exercise than the D rendezvous. This memo is to record a few of…
Descent Data Select procedures are finalized
On July 7 and 8 we held a final review of the Data Select procedures and Flight Controller interface during the Descent phase of the lunar landing mission. This lengthy memo is to describe briefly some of the items discussed, all of which are being thoroughly documented before the flight….
F mission rule regarding DPS gimbal drive failure indication
This memo is to report how it is currently planned to handle an indicated failure of the DPS gimbal drive actuator (GDA) on the F mission….
It is proposed that we plan a two step LOI maneuver
For the past several months there has been considerable discussion regarding the question of whether we should perform the lunar orbit insertion (LOI) maneuver as a single burn or if it should be made in two steps. This is an important matter to resolve since it has impact on RTCC program development, guidance systems targeting,…
RLS Determination
On April 2 we had a Mission Techniques meeting to discuss how we should handle the determination of the LMs position on the lunar surface (RLS). Specifically, we were concerned with how to determine its values and, after improved values are determined, when they should be loaded into the spacecraft computer. One obvious conclusion, if…
Some decisions regarding lunar landmark tracking on the F and G missions
We had an Ad Hoc Mission Techniques meeting on January 9 to talk over lunar landmark tracking. In particular, we wanted to discuss what we thought had been learned from the C’ mission and what we want to do on the F and G missions. This memo is to outline all that briefly. The specific…
All about F APS burn to depletion and landmark tracking
On February 14 we had a Mission Techniques meeting to pin down F lunar orbital operations between the end of rendezvous and TEI. Aside from a rest period, this consists of two exercises – the APS burn to propellant depletion and landmark tracking with the optics. I think we have a good understanding of how…
Operations required for communication loss on F and G are sure better than on C’
I think we have pretty well established how to handle a communication loss situation on the F and G missions. In effect, we have defined which Block data must be sent and what onboard cis-lunar navigation needs to be carried out. In both cases, of course, it is possible to cut back substantially from the…