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Study of solid rocket motors for a space shuttle booster. Volume 4: Mass properties report

A. H. Vonderesch

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Abstract

Mass properties data for the 156 inch diameter, parallel burn, solid propellant rocket engine for the space shuttle booster are presented. Design ground rules and assumptions applicable to generation of the mass properties data are described, together with pertinent data sources.

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What this paper is about

Mass properties data for the 156 inch diameter, parallel burn, solid propellant rocket engine for the space shuttle booster are presented. Design ground rules and assumptions applicable to generation of the mass properties data are described, together with pertinent data sources.

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Available abstract

Mass properties data for the 156 inch diameter, parallel burn, solid propellant rocket engine for the space shuttle booster are presented. Design ground rules and assumptions applicable to generation of the mass properties data are described, together with pertinent data sources.

Key concepts: Booster (rocketry), Solid-fuel rocket, Space Shuttle, Propellant, Aerospace engineering, Space launch, Propulsion, Environmental science

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