A propellant dynamic burning rate testing device
A technology of testing device and propellant, which is applied in the test of ammunition, ammunition, weapon accessories, etc., can solve problems such as propellant that has not yet been seen
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[0020] see figure 1 and figure 2 As shown, this embodiment presents a preferred structure of a propellant dynamic burning rate test device, including a body assembly, an ignition assembly, a first pressure sensor 8 , a second pressure sensor 13 and a data acquisition and processing system 16 .
[0021] The body assembly includes a body 6 , a first sealing plug 4 , a first gasket 5 , a second sealing plug 10 , a second gasket 11 and a moving burner 9 .
[0022] The body 6 has a multi-step through hole, from its left end to the right end (see figure 2 ) are threaded hole section 6-1, large-diameter hole section 6-3 and small-diameter hole section 6-5. A mounting hole 6-2; the large-diameter hole section 6-3 and the small-diameter hole section 6-5 transition through a 45° cone surface; the size of the small-diameter hole section 6-5 is Φ30mm×250mm and is at the junction of the 45° cone surface An annular positioning platform 6-4 is provided. A section of the outer wall of t...
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