Published October 14, 2015
| Submitted
Report
Open
Water Tunnel Tests of the M-6, 2.36" A. T. Rocket with Five Designs of Shroud Tail
- Creators
- Knapp, Robert T.
Abstract
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.
Additional Information
Office of Scientific Research & Development National Defense Research Committee. Division Six-Section 6.1. Section No. 6.1-Sr-207-934. HML Rep. No. ND-11.5.Attached Files
Submitted - ND-11.5.pdf
Files
ND-11.5.pdf
Files
(4.8 MB)
Name | Size | Download all |
---|---|---|
md5:544b7aa2de534be6f0a946dca96c3bc3
|
4.8 MB | Preview Download |
Additional details
- Alternative title
- Memorandum on Water Tunnel Tests of the M-6, 2.36" A. T. Rocket with Five Designs of Shroud Ring Tail
- Eprint ID
- 61127
- Resolver ID
- CaltechAUTHORS:20151014-162631419
- 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
- 50