Published October 14, 2015
| Submitted
Report
Open
Water Tunnel Tests of the M6, 2.36" A.T. Rocket
- Creators
- Knapp, Robert T.
Abstract
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.
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.Attached Files
Submitted - ND-11.4.pdf
Files
ND-11.4.pdf
Files
(4.6 MB)
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Additional details
- Alternative 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
- Eprint ID
- 61103
- Resolver ID
- CaltechAUTHORS:20151014-125552476
- OEMsr-207
- National Defense Research Committee
- Created
-
2015-10-14Created from EPrint's datestamp field
- Updated
-
2019-10-03Created from EPrint's last_modified field
- Caltech groups
- Hydrodynamics Laboratory
- Other Numbering System Name
- Hydrodynamics Laboratory
- Other Numbering System Identifier
- 48