Venting motor ejection charge on an electronically deployed rocket?
Hi there,
I have an idea to build a model rocket with an electronic servo driven parachute ejection system. however, where I live I am not able to obtain any plugged rocket motors with no ejection charge.
my current idea is to have the ejection charge vent through several small, symmetric side ports instead of pressurising the recovery bay.
Has anyone done this before? Is there any reason this wouldn’t work ( regarding side forces, stability, hot gas damaging the airframe?)
I would greatly appreciate any advice :)
Thanks!