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R. Meyer J. Köhler A. Homburg Explosives

R. Meyer J. Köhler A. Homburg Explosives

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23 Average Burning Rate<br />

front face open, in the tube and is packed tightly on all sides with coal<br />

dust. An incandescent spiral is placed in the cartridge opening; if the<br />

material is difficult to ignite (e.g. inverse salt-pair permissibles) the<br />

spiral is covered with a flammable igniter mixture. The tube is then<br />

closed by a perforated plate. The parameter measured is the minimum<br />

hole diameter at which the initiated deflagration arrives at the bottom<br />

of the cartridge.<br />

In a modification of the method two cartridges placed coaxially one an<br />

top of the other are tested.<br />

Aurol<br />

T-Stoff; Ingolin<br />

Concentrated (88–86%) hydrogen peroxide. It is employed in liquid<br />

fuel rocket engines as W Oxidizer or, after catalytic decomposition, as<br />

W Monergol. For its explosive properties, see Haeuseler, Explosivstoffe<br />

1, pp. 6–68 (1953).<br />

AUSTROGEL G1/G2<br />

Austrogel G1 and Austrogel G2 are a blasting cap sensitive gelatinous<br />

explosives. They do not contain any nitroaromatic compounds (W DNT<br />

or W TNT). The main ingredients are ammonium nitrate, nitroglycole<br />

and combustibles. Austrogel G1 and G2 may be used above and<br />

under ground. Austrogel G1 and G2 is also qualified very well as<br />

booster charge for low sensitive explosives such as W ANFO and<br />

other not cap sensitive explosives, and its manufactured by the Austin<br />

Powder GmbH, Austria (formerly Dynamit Nobel Wien)<br />

AUSTROGEL G1: AUSTROGEL G1:<br />

density: 1,5 g/cm3 1,45 g/cm3 oxygen balance: +4,0% +3,5%<br />

gas volume: 891 l/kg 881 l/kg<br />

specific energy: 1020 kJ/kg 1064 kJ/kg<br />

velocity of detonation: 6000 m/s 6200 m/s<br />

(steel tube confinement 52/60/500 mm)<br />

Average Burning Rate<br />

Mittlere Abbrandgeschwindigkeit; vitesse moyenne de combustion<br />

The arithmetic mean (statistical average) burning rate of pyrotechnic<br />

or propellants at specific pressures and temperatures. Dimension –<br />

length/time or mass/time.

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