Relays don't work very well in rocketry applications. Too much vibration and G forces.
and by the same standards, there are switches and phono jacks that fall in the same category
Relays don't work very well in rocketry applications. Too much vibration and G forces.
I hope that our meetings with the manufacturers will lead to something better defined than simply saying a physical break. We have to consider hardware, software/firmware, and how the devices operate in the absence of power, following a shutdown and restart, both intended and unintended. It doesn’t help that every device works a little or even a lot different.
And, yes, we understand that mischoosing or misusing a physical switch has its own problems also.
Not trying to add too much to your plate on this, but could you also address whether both legs of wires to an altimeter need switches in a mechanical switch arrangement? The standard-ish arrangement with one leg connected to the ematches with the other leg switched by the alt has always given me a few heebie-jeebies.
Okay but to that point then I could use a mag switch with an electromechanical relay wired into it?
Maybe, but for sure you want to do it with the battery disconnected... regardless of what switch you use.Perhaps I am off-base but we are acting as if altimeters and switches (and even e-matches) are the main issue,when it is the Gun Powder that is the concern.If this is the case,then perhaps ALL loading of gun powder should be done at an isolated spot,where the risk is rightly assumed by the TRA members and not the "civilians"
I humbly suggest that software/firmware/construction concerns might be addressed by manufacturer specified user tests and the user self-certifies that they have performed them for cases where the device can't self-test. RSO pre-inspection / retest optional. (I always assume that the RSO/club may set a stricter policy.)
I also humbly request that the Board consider establishing a minimum threshold where the policy applies, perhaps in terms of LPR/HPR. Impulse. Total grams of pyro charge. Grams of biggest single pyro charge. Or some combination.
1/2 gram of powder behind a 29mm nose cone will do a lot of damage if it hit someone.
However what if those MosFETs have gotten a static charge and have failed closed or whatever the cause is. Now you are down to a single point failure with no idea that it has happened.
The Scout leader that suffered a fatal injury at a non-TRA/NAR outing a few years ago was hit with a LPR on a 29mm motor. mv is a big number when v is big.
The Scout leader that suffered a fatal injury at a non-TRA/NAR outing a few years ago was hit with a LPR on a 29mm motor. mv is a big number when v is big.
Although a single mechanical switch (i.e., the relay contact) isolates the igniter, the activation circuit to that relay, at least in every controller I have seen, has at least two mechanical inhibits, typically a key switch and a push button. I would think dual inhibits in control of the relay would meet the overall safety intent.Playing devil's advocate again... why is power allowed to be connected to the launch control panel and/or pad boxes while flyers are loading? Particularly for the pad boxes (some of which may be wireless), there is only one "inhibit" in the loop... the device (relay or FET) that powers the igniter. And, they generally are allowed to have a continuity trickle current to the igniters.
Not necessarily true for all units. Some launch systems have processors (or wireless) and send a signal to the pad box to "fire channel 6". They don't directly connect to the relay coils from the control box.
Well, maybe RocketRev should chime in here as his wired and wireless systems are probably the most widely deployed (at least in the U. S.) for high power launches. I cannot believe he would design a launch system as you describe above.Not necessarily true for all units. Some launch systems have processors (or wireless) and send a signal to the pad box to "fire channel 6". They don't directly connect to the relay coils from the control box.
Most launch systems dont use software or electronic switches, once the key (in most cases a mechanically switched key is removed the power has no path to the igniter) and the launch button is a normally open mechanical switch as well.
Besides launch systems are not the subject of this thread.
Hence the reason I did not use "All"."Most" is not "All". There are "some" electronically-triggered systems that do not have a mechanical switch at the pad box, and therefore do not completely disconnect power to the leads.
And you are correct, launch systems are not the subject of this thread. The point was that not all energetic triggering systems that we use have a mechanical disconnect from power prior to connecting the igniter.
"Most" is not "All". There are "some" electronically-triggered systems that do not have a mechanical switch at the pad box, and therefore do not completely disconnect power to the leads.
And you are correct, launch systems are not the subject of this thread. The point was that not all energetic triggering systems that we use have a mechanical disconnect from power prior to connecting the igniter.
But the launch controller is; before you connect the leads to the igniter, it is as mechanically disconnected as you can get. And at that point it’s supposed to be on the pad in launch position which is completely compliant:
4.13.7 The function of firing circuits and onboard energetics shall be inhibited until the high power rocket is in the launching position.
.
My statement was that not all energetic triggering systems that we use have a mechanical disconnect from power prior to connecting the igniter. If the pad box does not have the battery disconnected or the power to the pad box is not physically shut off prior to loading, this is a correct statement. The igniter may be physically disconnected when you're loading, but once you connect it to the leads there might only be the switching circuitry coming between you and an accidental firing. Fortunately this is a very rare event.But the launch controller is; before you connect the leads to the igniter, it is as mechanically disconnected as you can get. And at that point it’s supposed to be on the pad in launch position which is completely compliant:
4.13.7 The function of firing circuits and onboard energetics shall be inhibited until the high power rocket is in the launching position.
.
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