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Water Tunnel Tests of the M6, 2.36" A.T. Rocket

Knapp, Robert T. (1943) Water Tunnel Tests of the M6, 2.36" A.T. Rocket. California Institute of Technology , Pasadena, CA. (Unpublished)

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This report covers Water Tunnel tests of a 2.36" rocket projectile with three types of shroud ring tail. Two of the tails are attached by channel section supporting fins to a stepped nozzle, the fins on one of them being stepped to fit the nozzle contour. The third tail has a streamlined nozzle with smooth supporting fins and shroud ring. The results are given of tests with different shroud lengths on the ring tails with the channel section supporting fins.

Item Type:Report or Paper (Technical Report)
Alternate Title:Memorandum on Water Tunnel Tests of the M-6, 2.36" A. T. Rocket Showing Comparison of Performance with the Conical Pointed Nose Combined with Three Types of Shroud Ring Tail and with Shroud Rings of Various Lengths
Additional Information:Office of scientific Research & Development National Defense Research Committee. Division Six-Section 6.1. Section No. 6.1-sr-207-920. HML Rep. No. ND-11.4.
Group:Hydrodynamics Laboratory
Funding AgencyGrant Number
National Defense Research CommitteeOEMsr-207
Other Numbering System:
Other Numbering System NameOther Numbering System ID
Hydrodynamics Laboratory48
Record Number:CaltechAUTHORS:20151014-125552476
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Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:61103
Deposited On:14 Oct 2015 20:00
Last Modified:03 Oct 2019 09:04

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