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FIRST STEPS TOWARD SPACE - Smithsonian Institution Libraries

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NUMBER 10 135<br />

FIGURE 2.—Model E rocket. From Oberth, Wege zur Raumschiffahrt, 1929.<br />

hydrogen-oxygen engines in propellant ratios of<br />

1:4 to 1:5 (instead of the stoichiometric ratio of 1:8)<br />

and produce exhaust velocities up to 5,000 m/sec.<br />

For the same reason, I proposed to add water to<br />

the alcohol in the first stages, even though these<br />

engines do not develop the high exhaust velocities<br />

of hydrogen-oxygen engines. Water has since been<br />

used in almost all engines burning alcohol. The<br />

demand for specifically heavier fuels in the first<br />

stages, even though they do not develop such high<br />

exhaust velocities, and for lighter fuels with higher<br />

exhaust velocities in upper stages, also resulted<br />

from the mathematical formulas in my writings.<br />

I tried to avoid static reinforcements by keeping the<br />

tanks under a light overpressure internally. This<br />

principle has been applied practically to the Atlas<br />

booster by Karel J. Bossart, who developed it to<br />

technical maturity. 10<br />

Another proposal of mine which has found application<br />

is the use of parachutes for landing rocket<br />

vehicles.<br />

Later on, I had proposed electricity for the steering<br />

mechanism. For example, for the speed-control<br />

system, I proposed that a mass should act against an<br />

elastic resistance; its deflection would then be a<br />

function of the acceleration. The mass was to act<br />

in such a way on a potentiometer (a variable electric<br />

resistor) that a current proportional to the acceleration<br />

would be produced. When this current is<br />

integrated, speed will be indicated. This instrument<br />

can also be used to close the fuel valves automatically,<br />

when the desired speed is reached.<br />

The attitude of the rocket was to be controlled<br />

by a gyroscope which caused the rudders to deflect<br />

by electric control as soon as the gyroscope and<br />

rocket axes were not parallel.<br />

In my book I also proposed a centrifuge, with<br />

an arm 35 meters long, to examine systematically<br />

the resistance of man to high accelerations, to train<br />

man at high accelerations, and to select among the<br />

applicants for space travel those with the best<br />

abilities.

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