Salami Rocket: Unterschied zwischen den Versionen

@@ Zeile 17: / Zeile 17: @@
 = Parts =
 [[Bild:Scaled-dscn9121.jpg|thumb|Overview of the rocket parts]]
-All parts directly participating in the combustion would have to sustain at least 51 bar (vapor pressure of N<sub>2</sub>0 at 20°C) but for reasons of safety i assume 200bar as the minimum.
+All parts directly participating in the combustion would have to sustain at least 51 bar
+(vapor pressure of N<sub>2</sub>0 at 20°C) but for reasons of safety i assume 200bar as the minimum.
 * [http://en.wikipedia.org/wiki/Pressure_vessel Run Tank]: A light-weight container for the oxydizer capable of sustaining enough pressure