So, with that said, I will continue to the best of my ability.
Last night, I met up with a friend from the MIT Rocket Team regarding the sensor placement in the Hermes III nosecone and we talked about the "screw-in" temperature sensors. Last Spring in the previous rocket design, we placed the sensors directly to the fiberglass body with Proline 4500 epoxy. This was troublesome because the fixture was basically permanent (until the high speed collision with the solid Mojave desert). This time, we will be able to strongly affix the sensors to the proper place in the nosecone but have the option to unscrew the sensors from the body.
Two weekends ago at Redbones BBQ in Davis Square
A dynamical signal analyzer helping me find Poles and Zeros in a second order modeled electro-mechanical system.