I want to build for myself an ultralight aircraft as it's my dream project since I was young. I plan to build the aircraft as a 10 years project so I want to plan out everything and know if it will be even possible first.
I live in Germany so I'll follow the European aviation regulations. The specs for the aircraft are: 200 kg MTOW, 120 kg empty weight, 80 km/h cruise speed, 50 km/h stall speed, 90 km/h max speed, 10 m wingspan, the aircraft use an electric turbofan engine provide 7 hp thrust. Currently, with the wind tunnel test I got L/D ratio of 15.22. Combine these elements give my aircraft estimated performance of 1.08 m/s climb rate and cruise range of 100 km.
So my question is: will this aircraft be suitable to fly in Germany? Since I've been here for quite a while, I understand how complex the German laws are. So I would also like to ask: if it's possible to register a complete self-build aircraft? My flight plan is quite simple, a local flight in VFR for recreational purpose. So the aircraft will fly mainly within unregulated airspace as for experimental aircraft. But my worry is also if it's possible to even register this aircraft for flying at all. So if anyone familar with this topic, I would appreciate the help.
Edit: So for the commends and the answer I recieved, I found many ask why I use a turbofan instead of a propeller. The aircraft I want to build will resemble a fighter jet, the F-117N Seahawk, that's why I want to mount the engine internally. At first I actually want to use a jet engine, but given the budget limit and the problem come with thermal and strutural of an ultralight, I decide to go with 2 turbofans for total of 12hp(I decide to add some margin for safety to the engine rated power of 7hp). Yes, I understand this design is very complex, will not as efficient as already established design and potentially not as good as I expected, but it's my dream project and if it meet at least the safety factor and have good enough performance, then I'll take it. I tried with many methode to increase the performance like: sharkfin winglets, blended body design, mainly use composite material like carbon fiber laminate,... which should help the final design performance to match the small prototype design I tested in CFD and wind tunnel.