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1972•NASA STI Repository (National Aeronautics and Space Administration)Open access

Study of solid rocket motors for a space shuttle booster. Volume 2, book 3: Cost estimating data

A. H. Vanderesch

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Abstract

Cost estimating data for the 156 inch diameter, parallel burn solid rocket propellant engine selected for the space shuttle booster are presented. The costing aspects on the baseline motor are initially considered. From the baseline, sufficient data is obtained to provide cost estimates of alternate approaches.

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Cost estimating data for the 156 inch diameter, parallel burn solid rocket propellant engine selected for the space shuttle booster are presented. The costing aspects on the baseline motor are initially considered. From the baseline, sufficient data is obtained to provide cost estimates of alternate approaches.

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Available abstract

Cost estimating data for the 156 inch diameter, parallel burn solid rocket propellant engine selected for the space shuttle booster are presented. The costing aspects on the baseline motor are initially considered. From the baseline, sufficient data is obtained to provide cost estimates of alternate approaches.

Key concepts: Booster (rocketry), Solid-fuel rocket, Space Shuttle, Propellant, Aeronautics, Aerospace engineering, Propulsion, Baseline (sea)

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Study of solid rocket motors for a space shuttle booster. Volume 2, book 3: Cost estimating data — Research Paper | ScholarLens