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 = | ||
Zeile 49: | Zeile 52: | ||
== 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] |
Version vom 16. Juni 2009, 16:02 Uhr
WTF?
Nomen est omen. Salami rocket is about building a hybrid rocket with a gaseous oxydizer and salami as propellants.
Oxydizer
I'd prefer N2O over 02 because although N2O carries a lot of conjectural inert nitrogen (64%) oxygen is much harder to handle (tank filling, storage & injection). Additionally the nitrogen, though not participating in combustion, raises the fuel erosion rate and cooles the nozzle enough to reuse it many times.
Fuel
Salami: High efficency hydrocarbon based fuel ;)
Draft
- Run Tank: A light-weight container for the oxydizer capable of sustaining enough pressure
- On/Off Valve: Enables/Disables oxydizer flow.
- Throttle valve: A valve to allow precise regulation of the oxydizer flow from the run tank to the combustion chamber.
- Injector: Aids in vaporizing the (still) liquid oxydizery.
- 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.
- 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
All parts directly participating in the combustion would have to sustain at least 51 bar (vapor pressure of N20 at 20°C) but for reasons of safety i assume 100bar as the minimum.
Run Tank
Smart Parts C02 aluminium tank for paintball guns with on/off valve.
- Capacity: 591ml (20 oz)
- Connector: 1,27cm (1/2")
- Max Pressure: 200bar
- Price: 45€
On/Off Valve
No separate valve needed since the proposed CO2 tank has it built-in.
Throttle valve
An adjustable throttle valve (Stasto VRB-030) intended for use in hydraulics.
- Connector: 1,27cm (1/2")
- Flow rate: 45 l/min
- Working pressure: 350 bar
- Price: 30€
Injector
Probably custom made. Basically a shower head ;).
Combustion Chamber
C02 aluminium tank for paintball guns without on/off valve.
- Capacity: 591ml (20 oz)
- Connector: 1,27cm (1/2")
- Max Pressure: 200bar
- Price: 14€
Nozzle
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.