Salami Rocket: Unterschied zwischen den Versionen

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(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/...)
 
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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?

Hybrid rocket propulsion system conceptual overview

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.


Links