Version vom 28. Juli 2009, 14:35 Uhr

WTF?

Hybrid rocket propulsion system conceptual overview

Schematic view of the "Donkey Power 1" salami rocket

3D view of the "Donkey Power 1" salami rocket

Nomen est omen. Salami rocket is about building a hybrid rocket with a gaseous oxydizer (N₂0) and salami as propellants.

Oxydizer

I'd prefer N₂O over O₂ 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. Most likely, since the alternatives i found are quite expensive, i will use the nitrous oxyde of whipped-cream chargers. By the way, never search for "Sahnespender" at google.

Fuel

Salami: High efficency hydrocarbon based fuel ;)

Simulation

Im using RockSim to simulate the flight stability of the rocket. The behaviour of the N₂0/Salami hybrid motor is simulated by an external model programmed in C++.

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 (parachute): Enables slow decent after burn-out for safety and reusability
Tail camera: It's all about the nice view
Altimeter: Measurement concludes the fate of the cat
Electric beacon: Transmits a signal to ease finding the landing site.
Filling system: Pipework to fill the run tank with nitrous oxyde from whipped cream chargers.

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 200bar 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 or this one -> SKR-54UC

Diameter: 54mm
Price: 53 €

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

SKR-54NZL graphite nozzle

Diameter: 54mm
Price: €35

Ignitor

None selected yet.

Shell

A nice design proposal by mactux. Exact specifications & blue prints yet to be made.

Recover System

None specified/selected yet.

Links

@@ Zeile 3: / Zeile 3: @@
 [[Image:DonkeyPower-schematic.jpg|thumb|Schematic view of the "Donkey Power 1" salami rocket]]
 [[Image:DonkeyPower1-3D.jpg|thumb|3D view of the "Donkey Power 1" salami rocket]]
-Nomen est omen. [http://en.wikipedia.org/wiki/Salami Salami] rocket is about building a [http://en.wikipedia.org/wiki/Hybrid_rocket hybrid rocket] with a gaseous [http://en.wikipedia.org/wiki/Oxidizing_agent oxydizer] and salami as propellants.
+Nomen est omen. [http://en.wikipedia.org/wiki/Salami Salami] rocket is about building a [http://en.wikipedia.org/wiki/Hybrid_rocket hybrid rocket] with a gaseous [http://en.wikipedia.org/wiki/Oxidizing_agent oxydizer] (N<sub>2</sub>0) and salami as propellants.
 = Oxydizer =

Salami Rocket: Unterschied zwischen den Versionen