See list attachedJUL 9 196868-PA-T-153APA/Chief, Apollo Data Priority CoordinationGood news on “C” mission SPS burns
The following is a verbatim copy of a note to me from Rick Nobles
(MPAD). I thought it worth distributing.
“The cross axis velocity errors resulting from SPS mistrim (CSM alone) will be about one half of what was previously anticipated. The reduction in error is due to the new DAP filter constants that the G&CD is recommending for the “C” mission erasable load. The only adverse effect is the mission planning that has been done to date.”
- Jul 25, 1968 – “D” MISSION RENDEZVOUS NAVIGATION MISSION TECHNIQUES PANEL (3.5σ)
- Oct 24, 1967 – Immediate restart of the SPS engine under PGNCS control (3.9σ)
- Dec 06, 1968 – C’ Abort Maneuver Overburn Monitoring (3.6σ)