Energy Aperture

Value chain · CLM-0984

In plain terms

The programme's own arithmetic for the antenna frame: each beam takes its length divided by five metres a minute plus twenty minutes to handle, which comes to about three hours per bay, padded to four for downtime.

The claim as recorded

NASA's 1981 construction summary derives the MPTS primary frame assembly rate as 4 hours per bay: 104 m and 147 m beams fabricated at 5 m/min plus 20 minutes handling each give 40.8 and 49.4 minutes per beam, 172 and 180.4 minutes per bay for the two beam machines, allowed as 3 hours per bay divided by a 75 per cent productivity factor, using two beam machines and four cherrypickers. The same summary takes equipment rates of 0.5 to 20 m/min as "assumed to be reasonable".

Evidence behind this: T3-programme summary, a derivation shown on one figure.

Scope and limits

ANTENNA PRIMARY FRAME ONLY; THE 20 MINUTES IS THE HUMAN SHARE OF A MACHINE-FABRICATED BEAM, NOT A MANUAL ASSEMBLY RATE. Table III-1 was cited by the text and has not been located and rendered. The 75 per cent productivity factor is ground rule [10] on p.12 (PDF 29), two pages before the rate range: "Construction operations will be performed during two 10-hour shifts per day and at 75 percent efficiency"; it is unexplained on the figure's page only.

What it assumes

The 75 per cent productivity factor is the source's and is unexplained on the page.

Where it comes from

SRC-465 Satellite Power System Concept Development and Evaluation Program, Volume VI: Construction and...
Figure III-39 from the render, "MPTS primary frame assembly equipment, sequence, and time line": "Assembly time: 104 m / 5 m/min + 20 min = 40.8 min; 147 m / 5 m/min + 20 min = 49.4 min; BM 1 3(40.8 min) + 49.4 min = 172 min/bay; BM2 2(40.8 min) + 2(49.4 min) = 180.4 min/bay; therefore allow 3 hr/bay / .75 = 4 hr/bay", with BM = beam machine and CP = cherrypicker, two beam machines (BM1, BM2) and four cherrypickers (CP1 to CP4) named on the sequence. p.12: "Construction equipment rates ranging from 0.5 to 20 m/min, shown in table III-1, are assumed to be reasonable. Low equipment use should be avoided." Arithmetic: 104/5 = 20.8, plus 20 is 40.8; 147/5 = 29.4, plus 20 is 49.4; 3 x 40.8 + 49.4 = 171.8; 2 x 40.8 + 2 x 49.4 = 180.4; 3/0.75 = 4.

Basis: hours per structural bay; beam metres per minute; handling minutes per beam

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

Cite this

energyaperture.com/c/clm-0984

CLM-0984, Energy Aperture, as of 1981.

Connected records

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

Also from SRC-465
CLM-0982The famous six months to build a satellite in orbit was decided first and the designs were fitted to it. One contractor says outright that...
CLM-0985By 1981 the programme put about four hundred people at the orbital construction base, with roughly two-thirds of them on the actual...
CLM-0987They built in high orbit not because it was cheaper - the 1978 numbers said low orbit was - but because a half-built satellite in low orbit...