I thought some people here might be interested in how I do avionics and deployments inside a minimum-diameter 38mm booster or 2nd stage rocket. I started doing it this way about 10 years ago, and it has worked well for me ever since.
To make the full multi-stage stack as rigid as I can, I minimize the number of airframe breaks. In my 3-stage 38 mm rocket I only have one for the booster/2nd stage separation, one for 2nd stage/sustainer separation, and one for sustainer deployments. I also prefer to separate stages immediately after burnout, to minimize drag losses. What this means for the 2nd stage is that there's an av-bay buried in the middle of the tube between 2 motors that needs to arm and ignite the 2nd stage motor on the aft end, fire a separation charge out the forward end, and then at apogee deploy a chute out the forward end also. In my rockets, the 2nd stage deployment hardware also needs to support the weight of the sustainer motor during the boost.
To make this easier, I use an N-shape floating av-bay structure that is deployed with the chute. Here is an av-bay for my booster that I made yesterday:
This is looking at the forward end, showing how the coupler tube is cut with an N-shaped cut, and the separation charge wiring. The open area where the wires are going is filled with the main chute and some harness. The connector is just a simple 0.1" pitch header male and female connector with wires soldered on and with heat-shrink tubing to provide some strain relief.
Here is the aft end, looking down at the top of the 38mm av-bay:
This photo was taken after I soldered on the brass nuts and the wires, and before I gooped it all up with JB Weld to glue the bulkhead in and strain relieve the wires. The bulkhead is a round circuit board I had made, that goes with the 38mm av-bay:
This av-bay provides power to the Raven via a magnetic switch. A tracker can also be squeezed into there if the battery and the Raven capacitor are moved over. It's 2" long. The active bulkhead with the power switch and battery charger are on the bottom and the top bulkhead just has passive electrical connections and is mostly there to provide structure and a place to attach the harness. The photo above is was taken before soldering anything on or gluing the top bulkhead into the structure.
Once the chute and harness is installed in the middle, inserting the parts into the airframe holds them together. The chute and the electronics are protected from the forward stage separation charge by the forward bulkhead, and then to deploy the chute, a deployment charge on the aft end of the av-bay ejects the whole thing forward and out of the rocket. The two pieces split apart and the chute falls out easily, without having to be extracted from a deep tube.
The photos above are what I'm using for the booster. But what about arming and igniting a 2nd stage motor? For the second stage I have the same basic hardware design, but add on a motor adapter piece that provides a screw switch for arming, a separation connector, and structural spacing between the motor and the deployable portion:
Shown in the photo above is the cylindrical motor ignition spacer and the round bulkhead which is attached to the back of the av-bay. The orientation is from the aft looking forward. On the top left is a 2-pin header connector that provides the separation between the av-bay and the motor igniter when the av-bay is ejected. On the top right is the arming screw switch. The two holes in the cylinder are for a 1.5" long aluminum female threaded spacer that goes through holes I drilled in the motor forward bulkhead and that screw into the airframe with 2 countersunk screws at both ends. The cylindrical part stays with the motor, and the round bulkhead is deployed as part of the av-bay. The cylinder also holds the av-bay deployment charge and harness. After I took this photo I glued the screw switch, wires, and header pins to the cylinder.
Here is another view of the rear bulkhead of the 2nd stage av-bay, with female 2-pin connector soldered on but not yet glued down:
On the left of the photo is a 1/4" round female-threaded spacer with #6 countersunk screws. I ended up using a narrower hex version so I could drill smaller holes through the end of the motor deployment bulkhead.
To make the full multi-stage stack as rigid as I can, I minimize the number of airframe breaks. In my 3-stage 38 mm rocket I only have one for the booster/2nd stage separation, one for 2nd stage/sustainer separation, and one for sustainer deployments. I also prefer to separate stages immediately after burnout, to minimize drag losses. What this means for the 2nd stage is that there's an av-bay buried in the middle of the tube between 2 motors that needs to arm and ignite the 2nd stage motor on the aft end, fire a separation charge out the forward end, and then at apogee deploy a chute out the forward end also. In my rockets, the 2nd stage deployment hardware also needs to support the weight of the sustainer motor during the boost.
To make this easier, I use an N-shape floating av-bay structure that is deployed with the chute. Here is an av-bay for my booster that I made yesterday:
This is looking at the forward end, showing how the coupler tube is cut with an N-shaped cut, and the separation charge wiring. The open area where the wires are going is filled with the main chute and some harness. The connector is just a simple 0.1" pitch header male and female connector with wires soldered on and with heat-shrink tubing to provide some strain relief.
Here is the aft end, looking down at the top of the 38mm av-bay:
This photo was taken after I soldered on the brass nuts and the wires, and before I gooped it all up with JB Weld to glue the bulkhead in and strain relieve the wires. The bulkhead is a round circuit board I had made, that goes with the 38mm av-bay:
This av-bay provides power to the Raven via a magnetic switch. A tracker can also be squeezed into there if the battery and the Raven capacitor are moved over. It's 2" long. The active bulkhead with the power switch and battery charger are on the bottom and the top bulkhead just has passive electrical connections and is mostly there to provide structure and a place to attach the harness. The photo above is was taken before soldering anything on or gluing the top bulkhead into the structure.
Once the chute and harness is installed in the middle, inserting the parts into the airframe holds them together. The chute and the electronics are protected from the forward stage separation charge by the forward bulkhead, and then to deploy the chute, a deployment charge on the aft end of the av-bay ejects the whole thing forward and out of the rocket. The two pieces split apart and the chute falls out easily, without having to be extracted from a deep tube.
The photos above are what I'm using for the booster. But what about arming and igniting a 2nd stage motor? For the second stage I have the same basic hardware design, but add on a motor adapter piece that provides a screw switch for arming, a separation connector, and structural spacing between the motor and the deployable portion:
Shown in the photo above is the cylindrical motor ignition spacer and the round bulkhead which is attached to the back of the av-bay. The orientation is from the aft looking forward. On the top left is a 2-pin header connector that provides the separation between the av-bay and the motor igniter when the av-bay is ejected. On the top right is the arming screw switch. The two holes in the cylinder are for a 1.5" long aluminum female threaded spacer that goes through holes I drilled in the motor forward bulkhead and that screw into the airframe with 2 countersunk screws at both ends. The cylindrical part stays with the motor, and the round bulkhead is deployed as part of the av-bay. The cylinder also holds the av-bay deployment charge and harness. After I took this photo I glued the screw switch, wires, and header pins to the cylinder.
Here is another view of the rear bulkhead of the 2nd stage av-bay, with female 2-pin connector soldered on but not yet glued down:
On the left of the photo is a 1/4" round female-threaded spacer with #6 countersunk screws. I ended up using a narrower hex version so I could drill smaller holes through the end of the motor deployment bulkhead.