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Rocket Tooling Poll


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Posted

For a while now I have wanted to poll the forum(s) about rocket tooling. I would like to develop a clearer sense of what tooling is being used for what, and where the red lines might start to be drawn.

What I would like to know:

1. Spindle dimensions (divergent, base of taper diameter, length of taper, end of taper diameter)
2. Drift dimensions (convergent, if relevant)
3. Propellants and loading pressures (etc) that you have used on said tooling (as descriptive as you are willing to be, please.)
4. Tube specification (manufacture, waxed/unwaxed)
5. Any other miscellaneous details that you will share about the construction.
6. I also would like to know about encountered failures, be it a CATO, or a rack roaster, and the tooling/propellant data to go along with it.

Thrust data is always good, but all observations are welcome.

donks

Posted (edited)

I`ll kick it off with a little one

 

0.5” id (short) coreburner

 

Spindle dimensions

Divergent: 30 degrees,

base of taper diameter: 7mm, length of taper: 45mm, end of taper diameter: 5.5mm

Drift 1: convergent : 45 degrees, Drift 2: flat

Propellant: hot 75/15/10 ball milled (willow) approx 9.8g, loading pressure: 5000psi

nozzle: 2.5g waxed bentonite clay.

Tube: ½” id x 1/8" wall x 3.34” (85mm) long. Unwaxed. Homemade using 90gsm pure kraftpaper + casein/dex glue.

 

Thrust Test Data (basic scale / vid cam + vid editing software):

Peak thrust: 3.55kg (7.826 lb) Total motor burn time: 0.568 seconds

Flight duration: 1.43 seconds

Very nippy with consistently reliable performance. Never had one cato so far.

 

https://youtu.be/Vrb0SQfwNfE

 

https://youtu.be/SneqZSKnRA4

Edited by Col
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