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R. Meyer J. Köhler A. Homburg Explosives

R. Meyer J. Köhler A. Homburg Explosives

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55 CDB Propellants<br />

Since W TNT is pourable at 80 °C (176°F), it is highly important in<br />

military technology. Since a considerable contraction takes place when<br />

the liquid explosive solidifies, good care must be taken during casting<br />

to ensure free access to all parts of the cast which have not yet<br />

solidified, in order to ensure proper replenishment of liquid material.<br />

Formerly, this was done by simple manual poking, but many automatic<br />

devices have been developed which do not involve any manual labor<br />

and which yield cavity-free casts.<br />

Pure TNT tends to form very long, needle-shaped friable crystals, with<br />

a loose texture which does not correspond to the maximum density.<br />

Cast TNT charges must be fine-crystalline, mechanically firm and<br />

dense, with numerous crystallization nuclei; i.e., solid TNT must be<br />

finely dispersed in the cast. According to BOFORS, the texture of the<br />

cast can be improved by the addition of W Hexanitrostilbene.<br />

Casting of Propellants<br />

Giessen von Triebsätzen; coulée de propergols<br />

Casting processes are needed especially in rocketry for the shaping of<br />

large propellant grains. Unlike in the casting of explosives, processes<br />

which cause shrinking and yield friable crystals cannot be applied.<br />

There are two solutions to this problem:<br />

a) hardening of polycondensates (e.g. polyurethanes or epoxys) with<br />

mechanically incorporated oxidizers, e.g. ammonium perchlorate<br />

(W Composite Propellants); the hardened plastic material acts as fuel<br />

for the oxidizer;<br />

b) converting of pourable nitrocellulose granules by treatment with<br />

liquid nitrate esters (e.g. with nitroglycerine). The granules can be<br />

poured dispersed in the liquid (“slurry casting”), or filled in the rocket<br />

motor shell and gelled in situ with the added nitrate ester.<br />

CDB Propellants<br />

W Composite Propellants.

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