This report covers tests on the M-6, 2.36" rocket with the conical pointed nose in combination with on experimental shroud ring toil from the Aberdeen Ballistic Research Laboratory, also with a commercially manufactured Ordnance Deportment shroud ring tail, and with three types of specially made model tails on which the shroud length was varied. One of the specially made model tails was mounted on a plain boom with no nozzle. All of the other tails were mounted on a stepped venturi nozzle
Resistance tests were conducted in the High Speed Water Tunnel on 2-in. diameter models of the 5-in....
The High Speed Water Tunnel is operated by the California Institute of Technology under Contract OEM...
Contract OEMsr-207 has been a project operated under Section 6.1 of the National Defense Research Co...
This report covers tests on the M-6, 2.36" rocket with the conical pointed nose in combination with ...
This report covers Water Tunnel tests of a 2.36" rocket projectile with three types of shroud ring ...
This report covers water tunnel tests of a 2.36" rocket projectile with several variations in profil...
This report covers tests of a 2" diameter model of the 7.2" Chemical Rocket to determine its perform...
This report covers water tunnel tests of a 2" diameter model of a 4.5" rocket projectile (designated...
This report covers the tests of a 2" diameter model of the 4. 5" H. E. Rocket, T38E3, to determine ...
The High Speed Water Tunnel is operated by the California Institute of Technology under Contract OE...
This report covers Water Tunnel tests made on a 2-inch diameter model of the Mk 53 Aircraft Depth Bo...
The High Speed Water Tunnel is operated by the California Institute of Technology under Contract OEM...
This report covers tests of a 2" diameter model of the 3.5" Rotating Rocket. Five different designs...
This report covers tests made on a 2-inch diameter model of the 5" spin-stabilized rocket. The tests...
High subsonic wind tunnel study of stability and control characteristics of antitank missile with ra...
Resistance tests were conducted in the High Speed Water Tunnel on 2-in. diameter models of the 5-in....
The High Speed Water Tunnel is operated by the California Institute of Technology under Contract OEM...
Contract OEMsr-207 has been a project operated under Section 6.1 of the National Defense Research Co...
This report covers tests on the M-6, 2.36" rocket with the conical pointed nose in combination with ...
This report covers Water Tunnel tests of a 2.36" rocket projectile with three types of shroud ring ...
This report covers water tunnel tests of a 2.36" rocket projectile with several variations in profil...
This report covers tests of a 2" diameter model of the 7.2" Chemical Rocket to determine its perform...
This report covers water tunnel tests of a 2" diameter model of a 4.5" rocket projectile (designated...
This report covers the tests of a 2" diameter model of the 4. 5" H. E. Rocket, T38E3, to determine ...
The High Speed Water Tunnel is operated by the California Institute of Technology under Contract OE...
This report covers Water Tunnel tests made on a 2-inch diameter model of the Mk 53 Aircraft Depth Bo...
The High Speed Water Tunnel is operated by the California Institute of Technology under Contract OEM...
This report covers tests of a 2" diameter model of the 3.5" Rotating Rocket. Five different designs...
This report covers tests made on a 2-inch diameter model of the 5" spin-stabilized rocket. The tests...
High subsonic wind tunnel study of stability and control characteristics of antitank missile with ra...
Resistance tests were conducted in the High Speed Water Tunnel on 2-in. diameter models of the 5-in....
The High Speed Water Tunnel is operated by the California Institute of Technology under Contract OEM...
Contract OEMsr-207 has been a project operated under Section 6.1 of the National Defense Research Co...