Scale model compressed air tests of 260-inch solid rocket with submerged nozzle to determine exhaust flow velocity and direction in annular channel
Investigation of a submerged nozzle for solid rockets
1967-01-01
Report
Keine Angabe
Englisch
INVESTIGATION OF A SUBMERGED NOZZLE FOR SOLID ROCKETS
AIAA | 1967
|Investigation of a submerged nozzle for solid rockets.
NTRS | 1967
|Online Contents | 2012
Online Contents | 1995