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Apollo 13 Moments of Interest / 003:56:32 TLI dynamics error shows Apollo 13 hurtling back to earth
« Last post by MadDogBV on January 22, 2025, 08:54:39 am »The DYNAMICS team Ray Reynolds and Bob Torres had a rough mission.
The Apollo 13 Mission Operations Report notes the following incident in the Problems & Resolutions section of FIDO's report:
The re-anchoring of the ephemeris on the pre-TLI vector also had the side effect of impacting multiple displays used by the MOCR personnel, including the CLAD - the command module looking angle display - which was used by the INCO to configure the high-gain antenna and also identify which spacecraft omni provided the best comm. At ~3:56 after the dynamics error, the CLAD was now showing the spacecraft Apollo 13 hurtling back towards the earth, because all the ephemeris knew was that 13 was still in orbit.
COMM Ed Fendell has a field day with this, delighting in embarrassing the FIDO over it. In the FIDO loop, Dave Reed is noticeably annoyed at DYNAMICS. "Mark yourself down for one," he orders them. Whether this is part of a disciplinary action or to buy Dave a beer later is unclear.
Link (COMM&INCO): https://apolloinrealtime.org/13/?t=003:56:32&ch=53
Link (FIDO): https://apolloinrealtime.org/13/?t=003:57:26&ch=20
The Apollo 13 Mission Operations Report notes the following incident in the Problems & Resolutions section of FIDO's report:
Quote
The SIVB LOX dump and evasive maneuvers were input to the RTCC at (approximately) 3:46:00. At this time, the Selects requested that the 2:59:00 zero ΔV maneuver (used for CSM separation attitude definition) be moved back to TLI cutoff. Dynamics was so instructed, however, TLI was moved instead. This resulted in the ephemeris re-anchoring on the pre-TLI CYI vector. This situation was ultimately corrected by deleting TLI and re-anchoring on CCHU08. (The consequence of this was to "turn on" the RTCC pre-TLI vent model. With this vent on, and unknown, later impact point evaluations with MSFC would not compare. It was not until 24 hrs later that the "vent on" situation was noted as having invalidated impact point comparisons attempted prior to a GET of approximately 6 hrs.)
The re-anchoring of the ephemeris on the pre-TLI vector also had the side effect of impacting multiple displays used by the MOCR personnel, including the CLAD - the command module looking angle display - which was used by the INCO to configure the high-gain antenna and also identify which spacecraft omni provided the best comm. At ~3:56 after the dynamics error, the CLAD was now showing the spacecraft Apollo 13 hurtling back towards the earth, because all the ephemeris knew was that 13 was still in orbit.
COMM Ed Fendell has a field day with this, delighting in embarrassing the FIDO over it. In the FIDO loop, Dave Reed is noticeably annoyed at DYNAMICS. "Mark yourself down for one," he orders them. Whether this is part of a disciplinary action or to buy Dave a beer later is unclear.
Link (COMM&INCO): https://apolloinrealtime.org/13/?t=003:56:32&ch=53
Link (FIDO): https://apolloinrealtime.org/13/?t=003:57:26&ch=20