This document contains several graphs and equations related to aerodynamics, control systems, and rocket thrust. The graphs show relationships between variables such as lift coefficient and angle of attack, burn rate and pressure, and thrust over time. The equations define terms like moment of inertia, transfer function for a control system, and burn rate as a function of pressure.

2. •
•
•
•
•

3. pss [rad / s]
pss [rad / s] Cl  0, 42
0,6
y = 0,0377x
0,4
CL
0,2
CL (linear)
CL (non…
1E-15
-3 2 7 12 17
-0,2 δ [deg]

4. •
• CHM

6. • ° °
• °

7. Ix
Iy, Iz

9. r (P)
Log (Burn rate)
 k 1

[mm/s]
1 1
20
A  k 1
*
k 1  Pe  k
 k  1    Pe  k 
      1  
Ae  2   P0   k  1    P0  
2 
 

1 10 100
Log (Pabs) [bar]

10. P u b l i c M i s s i l e s In tr u d e r
L a u n c h e d w i th [I3 1 5 _ a c c i a i o - 0 ]
800
700
600
500
T hrust N
400
300
200
100
0
0 ,0 0 ,1 0 ,2 0 ,3 0 ,4 0 ,5 0 ,6 0 ,7 0 ,8 0 ,9 1 ,0 1 ,1
T im e

11. X CP  X CG
1
D
Vwind  8 m/s

12. •
•

14. KI
Gc ( s)  K P   KD s
s

19. Roll angular speed [deg/s] 300 15
Fin deflection [degree]
200 10
100 5
0 0
Roll speed
-100 Fin deflection -5
Saturation
-200 -10
-300 -15
0 2 4 6 Time [s] 8 10
300 15
Roll angular speed [deg/s]
Fin deflection [degree]
200 10
100 5
0 0
-100 -5
-200 -10
-300 -15
0 0,5 1 Time [s] 1,5 2

20. Roll angular velocity
300
200 Unstabilized
Stabilized
100
[degree/s]
0
-100
-200
-300
-400
0 1 2 3 4 5 6 7 8 9 10
Time [s]
Roll angular position (integrated)
200
0
-200
-400
Degree
-600
-800
-1000
-1200
-1400
-1600
0 1 2 3 4 5 6 7 8 9 10
Time[s]

21. •
•
•
•
•
•