Energy Aperture

Value chain · CLM-0965

In plain terms

In 1973 an astronaut on Skylab put together two long poles from short sections in just over two hours, about six minutes per join. A 1975 antenna study used that as its only real-world data point for how fast people can build things in space.

The claim as recorded

Raytheon's 1975 MPTS study reports a measured Skylab 3 assembly rate - one astronaut assembled two 55 ft poles in 5 ft sections in 137 minutes, 6.2 minutes per operation - and projects 2.5 minutes per operation with a 90 per cent learning curve. Separately it states a tentative in-orbit fabrication rate of 420 lb/hr for MPTS structural elements, needing eight manufacturing modules to meet the assembly timetable.

T3 government or agency report · medium confidence · as of 1975-12 · past review · VER-1176 CONFIRMED 2026-09-17 · VC11

Evidence behind this: T3-primary-report carrying a T1 measurement: the Skylab 3 rate is an observed astronaut assembly time, the only measured human assembly rate in the corpus; the 420 lb/hr is modelled and the 2.5 min is a projection.

Scope and limits

THE SKYLAB FIGURE IS THE ONLY MEASURED HUMAN ASSEMBLY RATE IN THE HELD CORPUS AND IT IS A SUNSHADE POLE, NOT A STRUCTURAL MEMBER. The 420 lb/hr is "tentatively established" by an operations analysis, so modelled. The 2.5 min/op is a learning-curve projection. Three different standings in one paragraph; keep them apart.

What it assumes

"rain" is the text layer's rendering of "min" and "MI_rS" of "MPTS"; both transcribed raw, not repaired.

Where it comes from

SRC-451 Microwave Power Transmission System Studies, Volumes I to IV, December 1975, NASA-CR-134886,...
PDF p.175, raw rendering: "In the Skylab 3 mission, a single man assembled two 55 ft poles in 5 ft sections in 137 minutes. This represents an assembly rate of 6.2 rain/operation. A typical MI_rS 18 meter structural member would require 78 operations. Assuming a 90% learning curv_ improvement in skills relative to Skylab performance, a 2.5 rain/operation could be considered plausible." And: "An operations analysis of this process has tentatively established a rate of assembly of 420 lb/hr for the MPTS structural elements. At this rate, eight manufacturing modules would be required to meet assembly time tables." Arithmetic: two 55 ft poles in 5 ft sections is 22 sections; 137 / 22 = 6.23 min per operation, consistent with the stated 6.2.

Basis: minutes per assembly operation; lb per hour of structure

Related records
Answers question
QST-015 not published in this release

Cite this

energyaperture.com/c/clm-0965

CLM-0965, Energy Aperture, as of 1975-12.

Connected records

Other published records linked to this one. A list, not a judgement.

Also from SRC-451
CLM-0954The 1975 designers worked out how much their kilometre-wide antenna would bend, precisely so they could decide how good the beam-steering...
CLM-0959The original 1975 calculation found the satellite's radio noise would be fine for ordinary and troposcatter radio links and a problem only...
CLM-0960The 1975 study found the satellite's harmonics - the multiples of its transmit frequency - would trouble radio astronomy at the second and...
CLM-0961Everything in the 1975 interference analysis is for one satellite. The study itself says that a hundred of them would raise the noise and...
CLM-0966In 1975 the antenna alone was expected to take one to two years to assemble in orbit with about fifty people, and robot arms were judged...
CLM-0968The 1975 antenna study worked out how hot the middle of the transmitter gets depending on how efficient the tubes are and how tightly they...
CLM-0969If the tubes are only 70 per cent efficient, the transmitter's own face is not big enough to get rid of the heat they make, even spread...
CLM-0972If you take a 1975 estimate of how fast people could build structure in space, checked against one Skylab task, and apply it to the 1978...
More on the source page.