Salami Rocket: Unterschied zwischen den Versionen
Amir (Diskussion | Beiträge) |
Amir (Diskussion | Beiträge) |
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| Zeile 12: | Zeile 12: | ||
Im using [http://www.apogeerockets.com/RockSim.asp RockSim] to simulate the flight stability of the rocket. The behaviour of the N<sub>2</sub>0/ hybrid motor is simulated by an external model programmed in C++. | Im using [http://www.apogeerockets.com/RockSim.asp RockSim] to simulate the flight stability of the rocket. The behaviour of the N<sub>2</sub>0/ hybrid motor is simulated by an external model programmed in C++. | ||
[[Bild:Scaled-dscn9121.jpg|thumb|Over few of the rocket parts]] | |||
= Parts = | = 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. | ||