Usually when you see a 2-stage rocket, they expect you use a "special" motor for the bottom stage, one that doesn't have a delay for the deployment and also has the black powder (and not some "clay buckshot") at the deployment end. I've read elsewhere that not only does the method not have a delay, it also burns hotter when it burns through, which is part of why it ignites the 2nd stage...
My question is, if one were to use a lower-stage motor that is a traditional motor with a delayed ejection charge, would it ignite the second stage? (I know there's a secondary issue of the rocket wanting to go off at an angle if you have too long of a delay, but let's assume a short delay before the rocket has decelerated much, let's say 3 seconds or less)
and if it doesn't ignite the 2nd stage, does anyone know of a mechanism to trigger an igniter based on the prior stage's ejection charge? (My best thought to date was to trigger a relay based on a broken electrical connection when the lower-stage breaks away).
My question is, if one were to use a lower-stage motor that is a traditional motor with a delayed ejection charge, would it ignite the second stage? (I know there's a secondary issue of the rocket wanting to go off at an angle if you have too long of a delay, but let's assume a short delay before the rocket has decelerated much, let's say 3 seconds or less)
and if it doesn't ignite the 2nd stage, does anyone know of a mechanism to trigger an igniter based on the prior stage's ejection charge? (My best thought to date was to trigger a relay based on a broken electrical connection when the lower-stage breaks away).