FIRST STEPS TOWARD SPACE - Smithsonian Institution Libraries
FIRST STEPS TOWARD SPACE - Smithsonian Institution Libraries
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.