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Burn Wire Separation Mechanism? – September 2016

I was hoping to not use black powder charges that blow the rocket in half.

I know pyro recovery is light and simple, and generally pretty reliable. But it can be hard to test and I want to do something different. This might be a terrible idea.

Storing Energy

Fundamentally you need to store some energy to later use to separate the rocket. There aren’t too many options here, a gas generator (explosive), compressed air (like CO₂), and springs (rubber or metal). I figured I would look at metal springs since they can have very long lifetimes and be reasonably consistent. The goal isn’t to have the exact same ejection force every single time, but to have at least be above some threshold.

While thinking about this and looking around the internet I found this neat compact compression spring on McMaster Carr.

So I drew up a quick idea of a pair of blocks that would seat against the spring. One in the Nose (red) and one in the body tube. There is an inner tube for alignment (taking up side loads) and to keep things from tangling in the spring.

render

A quick FreeCAD drawing.

Release

At the very top there is an arch where a piece of monofilament line comes across the mechanism. This is tied to the base under load. The idea is you would compress the nose and body together and secure the line (somehow…). This would hold the rocket together in flight. At the tip of the device nichrome wire is wrapped around the monofilament line so that when heated the line breaks and releases the nose (at considerable force!) pulling out the parachute with it.

render

TODO: Design Issues