Presented at the C'Space 2011, Biscarosse, France.

2. Experimental Rocket Detrona

3. The CLES-FACIL

4. The CLES-FACIL
Space and aeronautics experimentations :
experimental rockets,CanSats, stratospheric balloons

5. The CLES-FACIL
Space and aeronautics experimentations :
experimental rockets,CanSats, stratospheric balloons
Since 1967 → important prize list, archives and
members network

6. The CLES-FACIL
Space and aeronautics experimentations :
experimental rockets,CanSats, stratospheric balloons
Since 1967 → important prize list, archives and
members network
20 to 30 active membres per year

7. The CLES-FACIL
Space and aeronautics experimentations :
experimental rockets,CanSats, stratospheric balloons
Since 1967 → important prize list, archives and
members network
20 to 30 active membres per year
International projects

8. Projects

9. Projects
Experimental Rockets

10. Projects
Experimental Rockets Stratospheric Balloons

11. Projects
Experimental Rockets Stratospheric Balloons Minirockets

12. Projects
Water Rockets Stratospheric Balloons Minirockets

13. Projects
Water Rockets PERSEUS rockets Minirockets

14. Projects
Water Rockets PERSEUS rockets CanSats

15. Rocket Detrona
Diametre : 120mm
Length : 1950mm
Total mass : 10kg

16. Rocket Detrona
Main experiences :
• Measurement of the constraints applied on the rocket by the parachute
Diametre : 120mm
Length : 1950mm
Total mass : 10kg

17. Rocket Detrona
Main experiences :
• Measurement of the constraints applied on the rocket by the parachute
• Rotating camera
Diametre : 120mm
Length : 1950mm
Total mass : 10kg

18. Rocket Detrona
Main experiences :
• Measurement of the constraints applied on the rocket by the parachute
• Rotating camera
• GPS
Diametre : 120mm
Length : 1950mm
Total mass : 10kg

19. Mesure de force
jauges de contrainte

20. Mesure de force
jauges de contrainte
Pont de Wheatstone complet :
V=G*V0*ε, (G=2, V0=5V)

21. Image stabilization

22. Image stabilization
• Objective : get a stable image by
compensating the rocket spin

23. Image stabilization
• Objective : get a stable image by
compensating the rocket spin
• Measurement of the rotation with an
accelerometer
Angular speed : ω=v/r=(a/r)1/2

24. Localization by GPS
Efficient way to locate the rocket after
landing.
Transmission of the GPS signal with an
868MHz radio emission and a ground
receptor
Both emitters and GPS systems are
located in the nose cone.

25. Thank you for your attention !