Salami Rocket: Unterschied zwischen den Versionen
Amir (Diskussion | Beiträge) |
Amir (Diskussion | Beiträge) |
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= 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. | |||
* [http://en.wikipedia.org/wiki/Pressure_vessel Run Tank]: A light-weight container for the oxydizer capable of sustaining enough pressure | * [http://en.wikipedia.org/wiki/Pressure_vessel Run Tank]: A light-weight container for the oxydizer capable of sustaining enough pressure | ||
* Throttle Valve: A valve to allow precise regulation of the oxydizer flow from the run tank to the [http://en.wikipedia.org/wiki/Combustion_chamber combustion chamber]. | * Throttle Valve: A valve to allow precise regulation of the oxydizer flow from the run tank to the [http://en.wikipedia.org/wiki/Combustion_chamber combustion chamber]. | ||