Salami Rocket: Unterschied zwischen den Versionen
Amir (Diskussion | Beiträge) Die Seite wurde neu angelegt: = WTF? = thumb|Hybrid rocket propulsion system conceptual overview Nomen est omen. Salami rocket is about building a [http://en.wikipedia.org/... |
Amir (Diskussion | Beiträge) Keine Bearbeitungszusammenfassung |
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* Combustion Chamber: Where the oxydizer/fuel mix burns. Additionally to pressure (same amount as for the run tank) it has to sustain heat. | * Combustion Chamber: Where the oxydizer/fuel mix burns. Additionally to pressure (same amount as for the run tank) it has to sustain heat. | ||
* Nozzle: An opening that dramatically accelerates the hot gas escaping the combustion chamber. | * Nozzle: An opening that dramatically accelerates the hot gas escaping the combustion chamber. | ||
* Ignitor: Preheating the fuel and initializing combustion. | |||
* Shell: Protecting the motor | |||
* Recovery System: Enables slow decent after burn-out for safety and reusability | |||
= Shopping list = | = Shopping list = | ||
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== Nozzle == | == Nozzle == | ||
Graphite laval nozzle that sustains up to 2000°C. No suitable model found yet. | Graphite laval nozzle that sustains up to 2000°C. No suitable model found yet. | ||
== Ignitor == | |||
None selected yet. | |||
== Shell == | |||
Nice proposal by [User:mactux mactux]. Exact specifications & blue prints yet to be made. | |||
== Recover System == | |||
None specified/selected yet. | |||
= Links = | = Links = | ||
* [http://en.wikipedia.org/wiki/Hybrid_rocket Basic concept of hybrid rockets at wikipedia] | * [http://en.wikipedia.org/wiki/Hybrid_rocket Basic concept of hybrid rockets at wikipedia] | ||
* [http://myweb.tiscali.co.uk/aspirespace/TechPapers.htm Excellent tech papers on calculating, planing and building hybrid rockets] | * [http://myweb.tiscali.co.uk/aspirespace/TechPapers.htm Excellent tech papers on calculating, planing and building hybrid rockets] | ||
