Aries

 

11/15/01

After weeks of preparation my newest project was ready today. This new project was a rocket different from all of my past engines. So what's so great about this rocket you ask? Well lets just say it's a 12" by 1" fire spitting behemoth. The casing was made of a 1" by 12" steel nipple available at all hardware stores. The bulk head consisted of a screw on end cap and the nozzle was made of the same thing, but I drilled a 1/4" hole for the nozzle throat. This is just a temporarily permanent device till I can machine a nozzle. I also wrapped some Teflon tape around the thread of both end to prevent gases to leak thorough the thread.

The fuel consisted of Potassium Nitrate (KNO3) and Fructose. These two ingredients were mixed with a ratio of 2 to 1 or 66% to 33%. The ingredients were mixed in a ziplock bag. To cast the propellant they are melted over a low flame while stirring constantly. If you don't stir it constantly the fructose will caramelize and performance will be reduced. To melt the propellant I used a Coleman propane stove, it is very convenient since it can be used out side so I don't upset my mother by heating up rocket fuel in the kitchen. Once adequately melted the propellant in poured into the casing with the bulkhead already attached. To form the core I used a 1/2" piece of dowel rod, I spin it frequently so it doesn't get "glued" in place by the propellant After the propellant set up, only and hour or so, the core rod it removed and the nozzle is then screwed on tightly.

On 11/14/01 I casted two engines of this design. The first one had a deferent nozzle than originally planned. This modified nozzle consisted of a reducer, down to 1/2", epoxy putty was then put in the reducer then shaped so to give it a de Laval design. The putty couldn't stand the heat or pressure exerted by the propellant and was completely blown out.

 

The second engine used the nozzle in the pictures above. It took a moment for it to build up thrust but when it did it was extremely loud and shot a smoke flume out about 30-40 feet, it was an impressive sight. The bulkhead and casing show no signs of stress of fatigue. The nozzle did expand slightly, but the area around the nozzle throat become discolored and be came thinner than it was. The burn time of 'full' thrust was about 1 second. All in all I am satisfied with the rocket, the casing and bulkhead can be reused, the nozzle however can't be but they are relatively cheap. Once I build an electronically deployed parachute I will further testing in actual rockets.

I don't currently have the resources to calculate or measure thrust or ISP, when I do I will be sure to update this page with that data.

If you have any questions you can e-mail me at Homer505@yahoo.com

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