A Test had been conducted testing the Electrical Ignition System and the engines ability to propel themselves against gravity
Rocket 1 (Small Relative Diameter)
Rocket 1 was a tremendous success!
there were some troubles with igniters failing to ignite, and the spinning caused by flawed aerodynamics and a misplaced nozzle, but overall it was a success
Further improvements are a nosecone and fins, I am looking into the possibility of 3d printing them
Now, Rocket 2 (Bigger Relative Diameter) is a different story
There were a few problems with this launch
First off, the igniters refused to work, resulting in me having to resort to a unreliable fuse, which worked after 2 attempts
The other problem is that it got stuck in the pipe, this is due to the larger diameter which is almost the same as the inner diameter as the large pipe, and the fact that the large pipe had a bend in it, causing it to collide with the inner walls and stop moving
FRIN (Further Research Is Needed) to prove whether or not this engine is worth making (Spoilers: it was not)
Overall this was great, and provided some much needed data
Next project is the Rocket Trust Testing Stand