SRC-499
Solar Power Satellite System Definition Study, Volume 5, Phase III Final Report: Space Transportation Analysis -- D180-25969-5; NASA CR-160746; June 1980
Boeing Aerospace Company (G. R. Woodcock named on the documentation form; subcontractors Grumman and Math Sciences Northwest) ·1980 · T3 government or agency report · VC02VC10
Commissioned by Lyndon B. Johnson Space Center, Contract NAS9-15636 (renders as "NAS9-16536"); technical monitor Harold Benson. Who paid for a study is recorded because it bears on how its conclusions should be read, not because it makes them wrong.
D180-25969-5; NASA CR-160746; no NTRS N-number printed on pp.1-4 the identifier this document is registered under
Published claims resting on this source
- CLM-1031 A launcher a third the size of the reference one would cost about a fifth more per kilogram to fly and need four launches a day instead of one, but would save five billion dollars up front and add only three per cent to the cost of each satellite. By 1981 everyone involved wanted it.
- CLM-1032 If the ferry's solar cells could not be repaired in flight it would wear out in three trips and the cost per kilogram would rise by about a third; thicker glass would fix that. A ten-minute delay restarting the engines every orbit cost more than the heat of being near Earth, and a chemical ferry would cost twice as much.
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SRC-499 , recorded 2026-09-17.