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Erosive Burning Phenomena

The above described phenomenon, known in the USA as .erosive burning, is called razgar in Russia and it is caused, accdg to D.K. Chernov (as quoted from Gorst,... [Pg.757]

This phenomenon is referred to as erosive burning. The extent of erosive burning depends on grain geometry and composition. Relatively "hot" propellants are apparently less subject to erosive burning than are "cool" ones. The inner surface of long tubes does not, apparently, burn in an even, uniform manner. The holes increase in size faster at the ends. Slotted tubes burn closely in conformance to Piobert s law. [Pg.229]

Burning, Erosive(in Propellants)(Erosive Effect of Gas Flow or Erosion of Propellants). Mansell (Ref 1) was one of the first to observe that the rate of burning inside tubular proplnts was faster than that on the outside. A similar phenomenon was observed later by Muraour(Ref 2). No importance was attached to this phenomenon until it was observed also(but on a larger scale) in rocket motors during and after WWII(Ref 11)... [Pg.357]

See other pages where Erosive Burning Phenomena is mentioned: [Pg.2]    [Pg.374]    [Pg.376]    [Pg.377]    [Pg.379]    [Pg.374]    [Pg.375]    [Pg.376]    [Pg.377]    [Pg.531]    [Pg.6]    [Pg.55]    [Pg.376]    [Pg.386]    [Pg.376]    [Pg.386]    [Pg.258]    [Pg.258]    [Pg.345]    [Pg.3]   


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Erosive burning

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