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R. Meyer J. Köhler A. Homburg Explosives

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End Burning Velocity<br />

the propellant; in liquid fuel and hybrid rockets, reignition can take<br />

place.<br />

End Burning Velocity<br />

Brennschlußgeschwindigkeit; vitesse en fin de combustion<br />

Velocity attained by a rocket at the moment at which combustion<br />

ceases. It is a function of the W Gas Jet Velocity, the W Mass Ratio,<br />

and the burning time.<br />

Endothermal<br />

Reaction that occurs with the absorption of heat (opposite of exothermal).<br />

Energetic Binders<br />

116<br />

Energetische Binder; Aktive Binder; active Binders<br />

In the realm of modern, nitric-ester-free W LOVA Gun Propellants, the<br />

widely used inert binders consume energy and to some extend have<br />

an undesirably high overall phlegmatizing effect on the explosivematerial.<br />

The high filler content of an explosive substance has a detrimental<br />

effect on the mechanical strength of this type of propellant.<br />

An active binder would be a preferable alternative if it combined a high<br />

energy content with favorable mechanical properties, together with a<br />

thermal stability higher than that of W Nitrocellulose or of W Polyvinylnitrate<br />

while remaining relatively uncomplicated to process.<br />

At present, the difficult task of developing such improved active binders<br />

has yielded only two usable compositions:<br />

1. W Polynitropolyphenylene, a non-crystalline explosive material that<br />

withstands high temperatures. This polymer is a gelatinous type of<br />

binder and is combined with small amounts of softeners, inert<br />

binders and W Hexogen or W Octogen. By means of organic solvents,<br />

it is processed into the corresponding LOVA composition.<br />

2. W Glycidyl Azide Polymer; a gas-producing glycerin derivate. The<br />

glycidyl azide polymer belongs to the group of reactivive polymers<br />

(thermoset materials) and is processed together with a main energy<br />

conductor, small amounts of softener, inert binders, curing<br />

agents and where necessary, accelerating agents. The type of<br />

acceleration and curing agents is determined not only by the final<br />

matrix structure, but also by the heat processing time of the respective<br />

composition and especially by the processing temperature.

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