Propuslion

NKP & Brown Sugar

We couldn't find KNO3 in any form, so I decided to use a blend/mix of NPK fertilizer and sugar.

I started mix and cook (heat to melt the sugar) them together to make a fuel paste as follows.

KNO3

Finally we found somewhere to buy KNO3 locally, after attempting to import it (in the form of Stump Remover) personally from the US and failed. So KNO3 was purchased on the 29th May, and I made a 65% KNO3 and 35% White Sugar mixture.

I am using KNO3: Potassium Nitrate (65% by weight) and Powder Sugar (35% by weight) to blend the rocket motor fuel. The burn was much more encouring. It was the exactly as I expected even before I amde rocket candy, but just a crystal state mixture.

The next moring I read more about KNO3 and Sucrose reactions trying to understand why everybody and everything I have read recommends 65%-35% ratio. I couldn't find it and then turned to a good old friend "Balanced chemical reactions" to the math hoping to get proof.

I found no proof. Instead, what I figured is the stoechiometric ratio is 73.925% of KNO3 and 26.075% of white sugar. I was surprized and puzzled more with the 65-35 ratio, but it reminds of the civil use Uranium and weapons grade Uranium.

I ran the test and found out that the 74% KNO3 -- 26% sugar mixture burns a bit more violently. It is the oxidizer rich vs 65-35 which is comperable to fuel rich in liquid rocket engines.

Rocket candy

Next I am making the comparison test of the two mixtures, but this time as candy (coocked). (I am also using toilet paper cores to make the motor case.)

I mixed two 100g of KNO3 and White Sugar. One in 0.65/0.35 another in 0.74/0.26 ratios.

I coocked them gently and made rocket candy of each configuration to measure the power to weight ration of each.

Then I packaged them in 9.7Cm long and 2.5cm diameter little tube. Net weight 57.7g for 74% KNO3 pack and 52.3g for the 65% KNO3 pack.

Latter we made bigger grains that we first test fired, and then packed in a 3D printed cylinder to make an engine, using the 65-35 raio. The ratio choice was because the simulation tool we were going to use "OPEN MOTOR" has preconfigured chemical mixture with that ratio.

Open Motor is an open source internal ballistics simulation software for rocket motor experimenters. And you can actually specify a new chemical's behaviour in the software to create new mixture. On that note we did a few modifications on KNSU preconfiguration of propellant mixture with one of my chemist friends (They can be different for you), but the default are good enough to work with from the get go.

This is the configuration we used from custom calculations and a bit of research and AI (Chat GPT) about KNO3-Sugar sugar mixtures and behaviours. The other reason to do this was because we didn't yet understand the difference between KNSU and KNSB, so we figured it could help to research on what we have and build around it.

These are the perfomance estimateds we had for our engine

These numbers were good enough to give our rocket a rapid lift on both of our flight attempts (watch the two videos on teh final project page).

The most important aspect of OpenMotor to me actually was the nozzle desigh part. That's what I was looking for when I found open motor, it was what open motor was built for primarily.

It allows you to play around with different nozzle geometries aspeects: Chamber radius and length, the same things for the Nozzle exit, and most importantly the throat parameters.

Project Development

    • KNO3: Potassium Nitrate & Sugar
      PVC Pipe
    • Processor: ESP32 DEVKIT-V1
      Data logger to SD Card
      Gyro & Accelerometer
      RF transmission
      Parachute Deployment
    • Body Tube
      Nose Cone: Electronics Housing
      Motor Gimbal: Thrust Vectoring
      Shock Cord
  • Contact

    Happy to receive your inquiries.

    Location:

    Kigali, Rwanda

    Call:

    +250 780 716 155