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FIRST STEPS TOWARD SPACE - Smithsonian Institution Libraries

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108 SMITHSONIAN ANNALS OF FLIGHT<br />

to be especially suitable: aniline and its mixtures<br />

with other aliphatic or aromatic compounds<br />

(triethylene-amine, cyclo-hexylamine,<br />

methylaniline, pyridine, ethylaniline, xylidine,<br />

piperidine, pyrrole). Certain mixtures show a<br />

"eutectic hypergolity." The hypergolity of the<br />

above mentioned compounds is so good that<br />

dilutions with inert fuels have been possible.<br />

The group of hypergoles mentioned was called<br />

by BMW "Tonka," and at Brunswick, "Gola."<br />

The BMW research staff conducted studies<br />

themselves in this field of hypergoles with excellent<br />

results (Figure 9).<br />

Unsaturated compounds: Substances belonging<br />

to the acetylene group (Dr. Reppe) as, for instance,<br />

di-acetylene. Vinyl-ethers: vinyl-ethylether,<br />

vinyl-isobutyl-ether, butane-diol-divinylether,<br />

divinyl-acetylene, diketenes, cyclo-pentadine.<br />

The hypergoles of the vinyl-ether group<br />

were called "Visoles" and were mostly used in<br />

combination with amino compounds.<br />

Developers: Pyrocatechol, hydroquinone, pyrogallol,<br />

and, in addition, "Optoles." The components<br />

suitable for hydrogen peroxide proved<br />

to be suitable also for nitric acid.<br />

Others: Furan and derivates, in particular fur-<br />

20<br />

-2<br />

10 sec<br />

15<br />

1<br />

CTS£L-<br />

qA><br />

Mean sci \tter of<br />

individua values<br />

M ethyl-anii ine<br />

100 80 20<br />

80<br />

+Am<br />

}-Am<br />

20 l>0 60<br />

Aniline<br />

loo<br />

FIGURE 9.—Ignition delays of the hypergolic fuel "Gola,"<br />

showing mean scatter of ten individual values.<br />

J<br />

furyl alcohol, called "Fantol" (Egelhaaf). They<br />

have particularly good hypergolity, especially<br />

with mixed acid, even when diluted to a high<br />

degree with xylol (up to 70 percent). Hydrazine<br />

also reacts hypergolically with nitric acid.<br />

Almost all proposed hypergolous propellants consisted<br />

of mixtures of different compounds. This results,<br />

of course, in a complication of the individual<br />

effects, yet mixing offers the possibility of intensifying<br />

one or the other of the desired properties, for<br />

instance, the chemical affinity of a mixture of two<br />

substances is in some way analagous to the solidification<br />

diagram of a system. Figure 10 shows this<br />

affinity expressed as a limit concentration, i.e., the<br />

acid concentration at which ignition takes place<br />

without perceptible delay. It can easily be understood<br />

that mixtures may have a considerably higher<br />

affinity than the single components, an effect which<br />

has also been proved true with numerous other substances.<br />

The same diagram shows the lowest admissible<br />

temperature, the so-called "cold point." This<br />

cold point is given at both ends of the diagram by<br />

the solidification point, in the middle by the highest<br />

admissible viscosity, which was assumed to be<br />

40 centi-strokes for a particular case. In this special<br />

case the optimum in regard to cold point as well<br />

as that to ignition delay are almost identical. There<br />

are, however, combinations of substances showing<br />

0 20 iO 60 80 % 100<br />

Aniline<br />

100 % 80 60 iO 20 0<br />

Cydo-hexylamine<br />

FIGURE 10.—Characteristic values of the hypergolic fuel system<br />

with aniline and cyclo-hexylamine, showing limit concentration<br />

(i.e., acid concentration up to which no delay is<br />

noticed.

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