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R. Meyer J. Köhler A. Homburg Explosives

R. Meyer J. Köhler A. Homburg Explosives

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Gas Generators<br />

Gas Generators<br />

gaserzeugende Ladungen; charges génératrices de gaz<br />

Pyrotechnic or propellant device in which propellant is burned to<br />

produce a sustained flow of gas at a given pressure on demand. Gasgenerating<br />

units are employed in blasting operations conducted in<br />

mines without recourse to brisant explosives. The device consists of a<br />

non-detonating gas-generating material and a priming or a heating<br />

charge, which are confined together in a steel pipe. The heating<br />

charge evaporates the gas-generating substance such as liquid CO2<br />

(W Cardox); another possibility is for the primer to initiate an exothermal<br />

chemical reaction (Chemecol process, Hydrox process). The<br />

gas-generating reaction may be the decomposition of nitrogen-rich<br />

compounds such as ammonium nitrate, or nitrate mixtures, or nitroguanidine<br />

in the presence of carbon carriers and sometimes in the<br />

presence of catalysts. When a given pressure has been reached, a<br />

bursting disc releases the gases in the pipe. The sudden gas expansion<br />

taking place in the borehole has an effect similar to that of an<br />

explosion.<br />

Gas Jet Velocity<br />

Nozzle Velocity; Ausströmgeschwindigkeit; vélocité à jet de gaz<br />

In rocket technology, the velocity of the combustion gases discharged<br />

from the combustion chamber and passing the nozzle into the atmosphere.<br />

The jet velocity and the mass flow serve to calculate the<br />

W Thrust. The jet velocity will increase with the pressure in the combustion<br />

chamber, i.e., with the expansion ratio under passage through<br />

the W Nozzle. The pressure in the combustion chamber should not be<br />

adjusted too high, otherwise the wall thickness of the chamber (i.e. its<br />

weight) will become too great (W Mass Ratio).<br />

In accordance with the Saint-Venant and Wantzel formula<br />

where:<br />

P0 is the gas pressure at the nozzle exit (atmospheric pressure);<br />

P1 is the pressure in the combustion chamber;<br />

k is the coefficient of specific heat;<br />

R is the ideal gas constant measured in absolute units;<br />

T is the flame temperature in Kelvin, and<br />

M is the mean molecular weight of the combustion gases.<br />

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