For abstract, see TN 15295 dup 15298100372ae274196a rpn NASA-CR-123613 rpn Rept-1917-MP1 cnt ctNAS8-28428 utl Mass properties report on 156-inch diameter SRM bas 1n13agn02057200018nenusususnnyfg3111aj000aa0a3h2280 foi HC csc 21h unc Analysis of mass properties data pertaining to solid propellant rocket engine selected for use with space shuttle booster mjs solid propellant rocket enginespropulsion system performancepropulsion system configurationsspace shuttle boosters mns engine designengine testssystems engineeringdata acquisition abs Mass properties data for 156-in.-dia SRM booster with two segments are presented. The SRM baseline booster has a fixed 15 degrees canted nozzle and no thrust neutralization system. Summary mass properties data for alternative booster configurations are included. (Author)
Feasibility Study of a Pressure-Fed Engine for a Water Recoverable Space Shuttle Booster
1972
121 pages
Report
Keine Angabe
Englisch