Add to ORKGThe cost data for solid propellant rocket engines for use with the space shuttle are presented. The data are based on the selected 156 inch parallel and series burn configurations. Summary cost data are provided for the production of the 120 inch and 260 inch configurations. Graphs depicting parametric cost estimating relationships are included
A systematic and standardized procedure for estimating life cycle costs of solid rocket motor booste...
Additional technical data have been prepared to supplement the data supplied in the SRM shuttle boos...
A study was conducted to analyze the characteristics and performance data for the booster vehicles t...
An analysis of the solid propellant rocket engines for use with the space shuttle booster was conduc...
Cost estimating data for the 156 inch diameter, parallel burn solid rocket propellant engine selecte...
A technical analysis of the solid propellant rocket engines for use with the space shuttle is presen...
The factors affecting the choice of the 156 inch diameter, parallel burn, solid propellant rocket en...
An analysis and design effort was conducted as part of the study of solid rocket motor for a space s...
A second iteration of the program baseline configuration and cost for the solid propellant rocket en...
The technical requirements for the solid propellant rocket engine to be used with the space shuttle ...
The study of solid rocket motors for a space shuttle booster was directed toward definition of a par...
Mass properties data for the 156 inch diameter, parallel burn, solid propellant rocket engine for th...
The baseline SRM design for the space shuttle employs proven technology based on actual motor firing...
A systems requirements analysis for the solid propellant rocket engine to be used with the space shu...
A study for the selection of a low cost shuttle system for design and development was conducted. The...
A systematic and standardized procedure for estimating life cycle costs of solid rocket motor booste...
Additional technical data have been prepared to supplement the data supplied in the SRM shuttle boos...
A study was conducted to analyze the characteristics and performance data for the booster vehicles t...
An analysis of the solid propellant rocket engines for use with the space shuttle booster was conduc...
Cost estimating data for the 156 inch diameter, parallel burn solid rocket propellant engine selecte...
A technical analysis of the solid propellant rocket engines for use with the space shuttle is presen...
The factors affecting the choice of the 156 inch diameter, parallel burn, solid propellant rocket en...
An analysis and design effort was conducted as part of the study of solid rocket motor for a space s...
A second iteration of the program baseline configuration and cost for the solid propellant rocket en...
The technical requirements for the solid propellant rocket engine to be used with the space shuttle ...
The study of solid rocket motors for a space shuttle booster was directed toward definition of a par...
Mass properties data for the 156 inch diameter, parallel burn, solid propellant rocket engine for th...
The baseline SRM design for the space shuttle employs proven technology based on actual motor firing...
A systems requirements analysis for the solid propellant rocket engine to be used with the space shu...
A study for the selection of a low cost shuttle system for design and development was conducted. The...
A systematic and standardized procedure for estimating life cycle costs of solid rocket motor booste...
Additional technical data have been prepared to supplement the data supplied in the SRM shuttle boos...
A study was conducted to analyze the characteristics and performance data for the booster vehicles t...