Pneumatic Rocket Parachute Deployment
Posted: Mon Sep 07, 2009 11:32 pm
Alright everyone, I have a slightly abnormal concept I am working on.
I am trying do design a cannon to be put inside a rocket, to pop off the nose cone, and eject the parachute. For reference, the usual method for ejecting the parachute in a model rocket, is a bit of loosely packed black powder, that explodes, pressurizing the entire body tube, popping the nose cone off.
This brings up several constraints that are usually not an issue with most of the stuff on this forum.
First off, it needs to be VERY light. I am talking about in the range of just a few ounces max.
Second, it needs to be SMALL. The entire device must fit in the 2" diameter body tube.
Third, it must be electronically activated, by the mini altimeter/computer I am working on.
Now moving on to the actual design.
What I am currently envisioning, is using a liquefied gas (probably either propane or butane, because CO2 is far too high pressure) to save on space.
The reason why using a liquid is so desirable is because a LOT of air is going to need to be released, in order to fill the body tube, and if the gas is liquified, at a low pressure such as propane or butane, you can get that high density, without extreme pressures.
The gas would in theory be held in with a burst disk, punctured by a solenoid, because a piston or ball valve would be far to heavy, and require more complicated electronics.
I was thinking the chamber could be easily filled if I were to use butane, and simply cut the end of a bic liter, to fill through. That way we could just fill it up right before the launch, in the field, with one of those lighter re-fillers.
Comments, questions, critiques, etc. all welcome.
edit: One last thing. The entire device must not have any sort of combustion, or pyrotechnics. The idea is to do it entirely non-pyro.
I am trying do design a cannon to be put inside a rocket, to pop off the nose cone, and eject the parachute. For reference, the usual method for ejecting the parachute in a model rocket, is a bit of loosely packed black powder, that explodes, pressurizing the entire body tube, popping the nose cone off.
This brings up several constraints that are usually not an issue with most of the stuff on this forum.
First off, it needs to be VERY light. I am talking about in the range of just a few ounces max.
Second, it needs to be SMALL. The entire device must fit in the 2" diameter body tube.
Third, it must be electronically activated, by the mini altimeter/computer I am working on.
Now moving on to the actual design.
What I am currently envisioning, is using a liquefied gas (probably either propane or butane, because CO2 is far too high pressure) to save on space.
The reason why using a liquid is so desirable is because a LOT of air is going to need to be released, in order to fill the body tube, and if the gas is liquified, at a low pressure such as propane or butane, you can get that high density, without extreme pressures.
The gas would in theory be held in with a burst disk, punctured by a solenoid, because a piston or ball valve would be far to heavy, and require more complicated electronics.
I was thinking the chamber could be easily filled if I were to use butane, and simply cut the end of a bic liter, to fill through. That way we could just fill it up right before the launch, in the field, with one of those lighter re-fillers.
Comments, questions, critiques, etc. all welcome.
edit: One last thing. The entire device must not have any sort of combustion, or pyrotechnics. The idea is to do it entirely non-pyro.