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Plan vs. actual: where Apollo 11 diverged from the script

A task-order and duration comparison between the pre-flight script — the Lunar Surface Operations Plan (LSOP, Final Edition, June 13 1969; nominal timeline sheets revised June 27) and the EVA Procedures (Final) — and the mission as flown, reconstructed from the Mission Report (§4.12 Lunar Surface Operations and Table 11-I, “Comparative times for planned lunar surface events,” p. 11-27 of the raw PDF), the Technical Crew Debriefing (§10), and the GET anchors in the annotated EVA timeline built from the air-to-ground transcript.

The crew did essentially everything the script called for, in nearly the scripted order — but almost nothing took the scripted time, and the whole moonwalk happened about 3½ hours earlier than the timeline page said it would. The three big divergences were (1) swapping the EVA ahead of the planned pre-EVA rest period, (2) an EVA prep that overran its simulation-derived estimate by about an hour, and (3) an unscripted ceremonial wedge — plaque, flag, presidential phone call — inserted into the middle of the timeline. Every task in the first two hours on the surface ran over plan; the schedule was recovered by sacrificing the lowest-priority item, the documented sample, exactly as the plan’s priority architecture intended. Total EVA still came in at the allotted ~2½ hours.

The LSOP (§3) laid out a ~22-hour stay structured as: post-landing checks → rest period → eat → EVA prep → a single two-man EVA of 2 h 40 min (cabin depress to repress) → post-EVA → a second 4 h 40 min rest → liftoff prep. Its nominal-timeline sheets put the EVA at 112:30–115:18 GET for the July 16 launch. The rationale section is explicit about the design philosophy: an early rest “before the strenuous pre-EVA, EVA, and post-EVA activities,” then a “slow, methodical” EVA with a gradual increase in task complexity, so that “should the EVA be terminated at any point in the timeline, the maximum data return for the time spent on the surface will be assured.”

That termination-proofing is the priority order: cabin-window photography → contingency sample → EVA evaluation → LM inspection → bulk sample → deploy experiments (EASEP + SWC) → documented sample. The companion EVA Procedures scripted only the cabin-side mechanics; its surface section just reads “EVA — Reference Lunar Surface Operations Plan.”

2. Before the surface script: the landing went off-book first

Section titled “2. Before the surface script: the landing went off-book first”

Context for everything that followed — covered in detail in powered descent and landing: the 1202/1201 program alarms pulled the crew’s attention inside the cockpit, Armstrong took manual control below ~1500 ft and flew ~1100 ft downrange of the aim point to clear West crater’s boulder field, touching down near the abort fuel limit. Two immediate surface consequences: the ground could not pinpoint Tranquility Base during the stay (the site was identified by matching the crew’s description of the avoided crater), and the LM came to rest with the MESA work table in deep shadow, which later taxed the bulk-sample collection. The Mission Report’s §4.12 also logs a post-landing surprise: the mission timer failed and was shut down 11 hours to cool (it recovered for ascent), and the descent-oxidizer venting had to be redone at ground request.

3. Divergence #1 — task order at stay level: EVA before rest

Section titled “3. Divergence #1 — task order at stay level: EVA before rest”

The single largest departure from the script was a deliberate one. The flight plan had the moonwalk between two rest periods; the crew had “given considerable thought” pre-flight to going early, and the conditions for it materialized: post-landing activities went cleanly, the crew wasn’t tired, and adaptation to 1/6 g was — per the debriefing — “very rapid and very pleasant.” The Mission Report (§4.12.2) records the decision time precisely: at 104:40:00 GET (about two hours after landing) the crew and ground agreed to proceed with the EVA before the first rest period.

Net effect on the clock: despite the prep overrun below, Armstrong was on the porch at 109:19:16 GET — roughly 3½ hours ahead of the LSOP timeline slot (depress scheduled at 112:30). The displaced rest period, taken after the EVA, was per the Mission Report “almost a complete loss” — cold suits, glycol-pump noise, light leaking through the shades; Aldrin slept fitfully for perhaps 2 hours, Armstrong not at all.

4. Divergence #2 — the hour-long EVA prep

Section titled “4. Divergence #2 — the hour-long EVA prep”

Preparation for the EVA began at 106:11:00 GET (Mission Report §4.12.2). Simulations had established 2 hours as a reasonable allocation; from prep start to Armstrong on the porch took about 3 hours 8 minutes. The overrun had three distinct causes, none of them the checklist itself (the crew: “we did, in fact, follow it pretty much to the letter”):

  • A real, cluttered cockpit. The simulator had only EVA gear, laid out in order. The flown cabin had “checklists, food packets, monoculars, and other miscellaneous items” — each forcing a small real-time decision about stowage or interference. The Mission Report’s verdict: prep “was conducted slowly, carefully, and deliberately, and future missions should be planned and conducted with the same philosophy.”
  • A known-bad connector. The RCU-to-PLSS 50-pin Bendix connector took at least 10 minutes per unit to mate — a problem “occasionally encountered using the same equipment before flight” (debriefing: a years-old, unfixed issue); at one point the crew doubted it would connect at all.
  • Depressurization through the bacteria filter — never fully rehearsed end-to-end on the ground — “took much longer than had been anticipated” (~30 minutes per the debriefing). Cabin pressure never indicated below 0.1 psi, and the hatch visibly bent as it was pulled open against the residual pressure. Table 11-I’s first row quantifies the tail end: “final preparation for egress” planned 10:00, actual 20:45, with ~8½ minutes spent between a 0.2-psia cabin reading and hatch opening.

5. Task order on the surface: the science spine held, with a ceremonial wedge

Section titled “5. Task order on the surface: the science spine held, with a ceremonial wedge”

Side by side, scripted sequence vs. the flown one (actual GETs from the EVA timeline):

#LSOP nominal sequenceAs flownDivergence
1Depress, CDR egressPorch 109:19, first step 109:24:48~3½ h early (rest skipped), prep long
2CDR environmental familiarizationDone, faster than planned
3Contingency sampleBagged 109:37Table 11-I: “performed out of sequence with planned timeline” (interleaved with photography)
4Preliminary LM checksDone”Out of sequence”
5LMP egressAldrin on surface 109:43On time (7:00 planned = 7:00 actual)
(not in nominal timeline)Plaque unveiling 109:52Unscripted insertion; interrupted TV deployment
6CDR redeploys TV to tripod sitePartial deploy interrupted, completed late+0:50 / +4:50 on the two phases
7LMP deploys Solar Wind CompositionDeployed 109:58Right slot, +2:20
(not in nominal timeline)Flag raised 110:09; President Nixon’s call 110:16Wholly unscripted; ~9 min absorbed into “LMP environmental familiarization”
8Bulk sample (CDR) + EMU evaluationSealed 110:35+4:15; scooping itself “about double the planned time”
9LM inspection (LMP, then CDR joins)Done+4:15 / +1:40; no abnormal conditions found
10EASEP offload + deploy (PSE, LRRR)Offload fast; deployed 111:02–111:12Offload −1:40, deploy +4:00 (leveling trouble)
11Documented sample, incl. core tubes111:16–111:26, cut to a grab-variety collection + 2 cores−16:10, “partially completed”
12SWC retrieval, pack/seal SRCsFoil rolled up 111:26Per plan
13LMP ingress → SRC transfer → CDR ingressHatch closed 111:39:13All under plan (0:00 / −5:00 / −3:16)

Two things stand out. The science spine ran in scripted order — contingency → bulk → experiments → documented, exactly the LSOP priority ladder. And the ceremonial block is invisible in the plan: neither the plaque nor the flag appears anywhere on the LSOP nominal-timeline sheets (even the June 27 revision), and the presidential call was a real-time insertion; Table 11-I books their cost as interruptions to the TV deployment and a +9:00 overrun on Aldrin’s “environmental familiarization” (“includes assisting Commander with plaque and television camera deployment”). See ceremonial surface activities.

6. Durations: Mission Report Table 11-I, planned vs. actual

Section titled “6. Durations: Mission Report Table 11-I, planned vs. actual”

Transcribed from the raw scan (MSC-00171, p. 11-27); times are min:sec.

EventPlannedActualΔTable’s remarks
Final preparation for egress10:0020:45+10:45~8 min 30 s from 0.2-psia cabin reading to hatch opening
Commander egress to surface10:008:00−2:00
Commander environmental familiarization5:002:05−2:55*
Contingency sample collection4:303:36−0:55Performed out of sequence with planned timeline
Preliminary spacecraft checks6:306:35+0:05Out of sequence
LMP egress to surface7:007:000:00~2 min 10 s for PLSS checks
Commander photography and observation2:40+2:40(no discrete planned slot)
TV camera deployment (partial)4:004:50+0:50Deployment interrupted for activity with plaque
LMP environmental familiarization6:0015:00+9:00Includes assisting Commander with plaque and TV camera deployment
TV camera deployment (complete)7:0011:50+4:50Includes photography of SWC and comments on surface characteristics
Solar wind composition deployment4:006:20+2:20
Bulk sample + EMU evaluation (complete)14:3018:45+4:15
LM inspection by LMP14:0018:15+4:15
LM inspection by Commander15:3017:10+1:40Includes closeup (ALSCC) photographs
Off-load experiment package7:005:20−1:40From SEQ-bay door open to door closed
Deploy experiment package9:0013:00+4:00Site selection to end of photography; trouble leveling the equipment
Documented sample collection34:0017:50−16:10Partially completed
LMP ingress4:004:000:00
Transfer sample return containers14:009:00−5:00
Commander ingress9:306:14−3:16Includes cabin repressurization

* The scan prints −2:00; −2:55 is the arithmetic of the planned/actual cells. The scan is rough; values were cross-checked planned + Δ = actual where legible.

The pattern: essentially everything from hatch-open through experiment deployment ran over — small overruns from deliberateness and dust, large ones from the unscripted ceremonies (+9:00) and the EASEP leveling fight (+4:00; no horizon reference, ineffective 1/6-g balance cues, scraping soil to change an instrument’s slope). The whole deficit was then repaid in one place: the documented sample, the plan’s own lowest-priority item, cut from 34 to ~18 minutes. Per §4.12: “Insufficient time remained to take the documented sample, although as wide a variety of rocks was selected as remaining time permitted” — plus two core tubes that could only be driven ~6 inches into unexpectedly hard subsurface (the hammer missed several times). Closeout, by contrast, beat the plan across the board. From porch to hatch-close took ~2 h 20 min; the Mission Report books the surface exploration as completed within the allotted ~2½ hours.

7. The surprises the plan couldn’t have scripted

Section titled “7. The surprises the plan couldn’t have scripted”
  • Dust as a system problem. The “graphite-like” powder coated the LEC straps until the conveyor bound and rained dust into the cabin (“we all looked like chimney sweeps”), made the ladder slippery, hid the white TV cable (which kept snaring Armstrong’s feet), and forced ~20 sunlit trips for the bulk sample because the MESA sat in deep shadow — see regolith and soil mechanics.
  • A two-layer surface. Soft fines over a hard substrate: core tubes stopped at ~6 in, the SWC staff and flagstaff penetrated only 4–5 in, and the PSE bubble level wouldn’t settle.
  • The body worked better than predicted. Metabolic rates ran lower than expected (§10); gravity subjectively “felt closer to one-tenth”; the natural gait was an unplanned lope. The crew’s recommendation: future crews can take on more.
  • An accidental first seismic calibration. The jettisoned PLSS backpacks hit the surface and the just-deployed seismometer registered the shocks — an unplanned end-to-end test of the instrument.
  • Small breakages. A cockpit circuit breaker snapped off against a PLSS during post-EVA movement (§16.2.11); the sample boxes took “great force” to seal; voice dropouts inside the cabin pre- and post-EVA never recurred outside.

8. What held: the plan’s architecture absorbed its own failure

Section titled “8. What held: the plan’s architecture absorbed its own failure”

The deepest finding is that the LSOP diverged everywhere in detail and nowhere in structure. Its two governing ideas — priority-ordered tasks (“maximum data return for the time spent”) and a conservative, buildup-paced timeline — are precisely what let a late prep, an early start, a presidential phone call, and a dozen small overruns end with: all five priority-list items above the documented sample fully accomplished, all three experiments deployed and working, ~21 kg of samples sealed and transferred, hatch closed at 111:39:13, and liftoff on schedule at 124:22 GET after a 21.6-hour stay against the ~22 planned. The only casualties were the full documented-sample protocol — and a night’s sleep.