The different parameters in the launch of a model rocket shall be verified using a motor test stand, rocket flight simulation and test launches with sensors on board. The results shall be presented during the 2024 DLA Launch Day.
# Project goals
- [ ] Develop and build a rocket motor test stand
- [ ] Verify the thrust curves of standard 18 mm motors
- [ ] Build and simulate a 35 mm model rocket to verify flight curves
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@@ -20,7 +21,7 @@ A standard 35 mm model rocket shall be used in test flights and simulation: [Lis
## Flight phases
Model rocket flights can be divided into different flight states [[1](https://code.fbi.h-da.de/hda10343/dla/-/wikis/Altimeter#sources)]:
Model rocket flights can be divided into different flight states \[[1](https://code.fbi.h-da.de/hda10343/dla/-/wikis/Altimeter#sources)\]:
The sensor platform that was developed in [previous projects](2023 Altimeter WLAN) shall be used for in-flight data recording. It shall be modified if necessary (hardware and software).
The sensor platform that was developed in [previous projects](2023%20Altimeter%20WLAN) shall be used for in-flight data recording. It shall be modified if necessary (hardware and software). 
* Wahl der Kraft/Druck-sensoren bzw. Anzahl der zu benutzende Sensoren. (Je mehr der Motor stark ist , desto grösser wird der Anzahl an Sensoren sein )
* Wahl der Temperatur-Sensoren (Sensoren zur Messung der Temperatur innerhalb des Motors und der umgebenden Umgebung )
* Steuerelektronik für die Aktivierung und Deaktivierung des Motors