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Swell Sleeves for Testing Explosive DevicesA method of testing explosive and pyrotechnic devices involves exploding the devices inside swell sleeves. Swell sleeves have been used previously for measuring forces. In the present method, they are used to obtain quantitative indications of the energy released in explosions of the devices under test. A swell sleeve is basically a thick-walled, hollow metal cylinder threaded at one end to accept a threaded surface on a device to be tested (see Figure 1). Once the device has been tightly threaded in place in the swell sleeve, the device-and-swell-sleeve assembly is placed in a test fixture, then the device is detonated. After the explosion, the assembly is removed from the test fixture and placed in a coordinate-measuring machine for measurement of the diameter of the swell sleeve as a function of axial position. For each axial position, the original diameter of the sleeve is subtracted from the diameter of the sleeve as swollen by the explosion to obtain the diametral swelling as a function of axial position (see Figure 2). The amount of swelling is taken as a measure of the energy released in the explosion. The amount of swelling can be compared to a standard amount of swelling to determine whether the pyrotechnic device functioned as specified.
Document ID
20110023590
Acquisition Source
Johnson Space Center
Document Type
Other - NASA Tech Brief
Authors
Hinkel, Todd J.
(NASA Johnson Space Center Houston, TX, United States)
Dean, Richard J.
(NASA Johnson Space Center Houston, TX, United States)
Hohmann, Carl W.
(NASA Johnson Space Center Houston, TX, United States)
Hacker, Scott C.
(NASA Johnson Space Center Houston, TX, United States)
Harrington, Douglas W.
(NASA Johnson Space Center Houston, TX, United States)
Bacak, James W.
(Lockheed Engineering and Sciences Co. Houston, TX, United States)
Date Acquired
August 25, 2013
Publication Date
February 1, 2003
Publication Information
Publication: NASA Tech Briefs, February 2003
Subject Category
Man/System Technology And Life Support
Report/Patent Number
MSC-23306
Distribution Limits
Public
Copyright
Public Use Permitted.
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