אבל כן זה מבוסס על קובץ AIM 9 עם לזה התכוונתה
#----------------------------------------------------
# Rafael Python 4
#----------------------------------------------------
# Final Time (sec)
60.000000
# Pk (0.0-1.0)
1.000000
# Weight of missile (lbs)
228.00
# Weight of propellant (lbs)
100.00
# Motor Impulse (lb-sec)
12610.000000
# Reference Area (ft*ft)
0.2164
# Nozzle Exit Area (ft*ft)
0.12985
# Length (ft)
6.42
# AOA max (deg)
30.00000
# AOA min (deg)
-30.00000
# Beta max (deg)
30.00000
# Beta min (deg)
-30.00000
# Velocity min (Mach)
0.500000
# Gimbal Angle Limit (deg)
90.0
# Gimbl Ang Rate Lim (deg/sec)
90.0
# Field of View (deg)
4.00
# Guidance Delay
0.250
# Lofting Bias
0.000000
# Proportional nav gain
2.400000
# Autopilot Bandwidth
0.000000
# Time To Go Active (sec)
-1.000000
# Seeker Type, Version
0 11
# Display
0
# Missile loft time
10.00000
# boostguidesec
0.50000
# terminalguiderange
6076.000
# boostguideSensorPrecision
3.600000
# sustainguideSensorPrecision
3.100000
# terminalguideSensorPrecision
2.400000
# boostguideLead
2.000000
# sustainguideLead
1.000000
# terminalguideLead
1.000000
# boostguideGnav
1.000000
# sustainguideGnav
1.500000
# terminalguideGnav
2.100000
# boostguideBwap
0.070000
# sustainguideBwap
0.060000
# terminalguideBwap
0.050000
#
# Python 4 BASIC AERODYNAMIC COEFFICIENTS
#
#
# MACH BREAKPOINTS
#
#MACH
11
0.0 0.4 0.8 0.95 1.05 1.2 1.6 2.0 3.0 4.5 6.0
#
# ALPHA BREAKPOINTS
#
#ALPHA
8
0.0 4.0 8.0 12.0 16.0 20.0 24.0
32.0
#
# Normal Multiplier
1.35
# NORMAL FORCE COEFFICIENT CZ (SYMMETRIC ABOUT ALPHA = 0)
#
#Mach 0.0
0.00 -2.12 -5.35 -8.80 -12.00 -16.00 -19.84 -23.63
#
#Mach 0.4
0.00 -2.30 -5.81 -9.57 -13.04 -17.39 -21.57 -23.63
#
#Mach 0.8
0.00 -2.65 -6.69 -11.00 -15.00 -20.00 -24.08 -28.00
#
#Mach 0.95
0.00 -3.78 -9.56 -15.71 -21.43 -28.57 -35.43 -40.00
#
#Mach 1.05
0.00 -3.78 -9.56 -15.71 -21.43 -28.57 -35.43 -40.00
#
#Mach 1.2
0.00 -2.65 -6.69 -11.00 -15.00 -20.00 -24.08 -28.00
#
#Mach 1.6
0.00 -3.31 -8.36 -13.75 -18.75 -25.00 -31.00 -35.00
#
#Mach 2.0
0.00 -3.53 -8.92 -14.67 -20.00 -26.67 -33.07 -37.33
#
#Mach 3.0
0.00 -3.68 -9.29 -15.28 -20.83 -27.78 -34.44 -38.89
#
#Mach 4.5
0.00 -3.78 -9.56 -15.71 -21.43 -28.57 -35.43 -40.00
#
#Mach 6.0
0.00 -3.89 -9.83 -16.18 -22.06 -29.41 -36.47 -41.17
#
#
# AXIAL FORCE COEFFICIENT CX (SYMMETRIC ABOUT ALPHA = 0)
#
# Axial Multiplier
3.0
#
#Mach 0.00
-0.10 -0.09 -0.08 -0.06 -0.04 -0.01 -0.008 -0.015
#
#Mach 0.40
-0.11 -0.10 -0.08 -0.06 -0.05 -0.03 -0.014 -0.013
#
#Mach 0.80
-0.12 -0.11 -0.09 -0.07 -0.05 -0.03 -0.016 -0.015
#
#Mach 0.95
-0.17 -0.16 -0.13 -0.10 -0.07 -0.04 -0.02 -0.021
#
#Mach 1.05
-0.24 -0.22 -0.18 -0.14 -0.10 -0.06 -0.029 -0.03
#
#Mach 1.20
-0.41 -0.37 -0.31 -0.23 -0.17 -0.102 -0.05 -0.051
#
#Mach 1.60
-0.38 -0.35 -0.29 -0.238 -0.16 -0.102 -0.049 -0.051
#
#Mach 2.00
-0.348 -0.32 -0.261 -0.203 -0.145 -0.09 -0.042 -0.043
#
#Mach 3.00
-0.32 -0.28 -0.24 -0.18 -0.12 -0.07 -0.04 -0.03
#
#Mach 4.50
-0.30 -0.28 -0.23 -0.18 -0.13 -0.08 -0.04 -0.038
#
#Mach 6.00
-0.32 -0.30 -0.24 -0.19 -0.14 -0.08 -0.04 -0.040
#
#
#
# Engine Data
#
#
# BURN TIME BREAKPOINTS
#
# BRNTIM
12
0.000 0.025 0.400 1.200 3.000 4.000 5.000
6.600 6.700 6.800 6.850 6.900
#
# ENGINE THRUST (LBS)
#
# THRST1
0.0 7000.0 1800.0 1800.0 2800.0 3000.0 3400.0
3600.0 3200.0 1200.0 600.0 0.0
#
#
# Range Data (generated by Missile Test Program)
#
#
# Table Multiplier
1.0
# Number of altitude breakpoints:
6
# Altitude breakpoints:
0.0 10000.0 20000.0 30000.0 40000.0 50000.0
# Number of Velocity breakpoints:
2
# Velocity breakpoints:
0.00 1181.49
# Number of Aspect breakpoints:
3
# Aspect breakpoints:
0.0000 1.5708 3.1416
# Alt = 0
# Vel = 0.00
18000.00 12000.00 9000.00
# Alt = 0
# Vel = 1181.49
20000.00 12000.00 11000.00
# Alt = 10000
# Vel = 0.00
19000.00 15000.00 10000.00
# Alt = 10000
# Vel = 1181.49
22000.00 15000.00 13000.00
# Alt = 20000
# Vel = 0.00
20000.00 17000.00 12000.00
# Alt = 20000
# Vel = 1181.49
24000.00 17000.00 15000.00
# Alt = 30000
# Vel = 0.00
22000.00 18000.00 15000.00
# Alt = 30000
# Vel = 1181.49
26000.00 18000.00 18000.00
# Alt = 40000
# Vel = 0.00
24000.00 19000.00 18000.00
# Alt = 40000
# Vel = 1181.49
28000.00 26000.00 22000.00
# Alt = 50000
# Vel = 0.00
26000.00 26000.00 20000.00
# Alt = 50000
# Vel = 1181.49
30000.00 28000.00 26000.00
maxGTerminal 70
maxGNormal 70
foxType 2
נערך לאחרונה: לפני 18 שנים
