Study of solid rocket motors for a space shuttle booster. Volume 2, book 3, addendum 1: Cost estimating data
A. H. Vonderesch
Abstract
Open-access reader
A. H. Vonderesch
Abstract
Open-access reader
A second iteration of the program baseline configuration and cost for the solid propellant rocket engines used with the space shuttle booster system is presented. The purpose of the study was to ensure that total program costs were complete and to review areas where costs might be overly conservative and could be reduced. Labor and material were analyzed in more depth, more definition was prepared to separate recurring from nonrecurring costs, and the operations portions of the engine and stage were separated into more identifiable activities.
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A second iteration of the program baseline configuration and cost for the solid propellant rocket engines used with the space shuttle booster system is presented. The purpose of the study was to ensure that total program costs were complete and to review areas where costs might be overly conservative and could be reduced. Labor and material were analyzed in more depth, more definition was prepared to separate recurring from nonrecurring costs, and the operations portions of the engine and stage were separated into more identifiable activities.
Key concepts: Booster (rocketry), Solid-fuel rocket, Space Shuttle, Propellant, Addendum, Aeronautics, Aerospace engineering, Space launch