[delX/100] 1 I 0 13 0
[dely/20] 2 I 0 15 0
[V/1000] 3 I 11 0 0
[theta] 4 I 0 10 0
[Vsq/10^6] 5 X 3 3 0
[sin_theta] 6 S 4 0 0
[cos_theta] 7 C 4 0 0
[Y_>_4] 8 O 2 0 0
[ct/V] 9 / 7 3 0
[Tdot@Y>4] 10 R 8 9 0
[Vdot@Y>4] 11 R 8 12 0
[Vdot/1000] 12 W 5 6 0
[delVdot/1000] 13 O 14 0 0
[Xdot/1000] 14 X 3 7 0
[Ydot/1000] 15 X 3 6 0
[-delX/100] 16 + -1 0 0
[-delY/20] 17 + -2 0 0
[-X>60] 18 O 16 0 0
[Y<14]] 19 O 17 3 0
[Hit<14] 20 & 8 18 19
[Splat] 21 F 20 0 0
[Yplane] 22 1 1 0 0
#
* 1 0.0 10.0 0.0 100. 0.0
* 2 0.0 50.0 0.0 20. 0.0
* 3 0.890 0.0 0.0 1000. 0.0
* 4 0.04352 -0.0322 0.0 1.0 0.0
* 5 0.0 0.0 0.0 1.0e06 0.0
* 6 0.0 0.0 0.0 1.0 0.0
* 7 0.0 0.0 0.0 1.0 0.0
* 8 -0.2 0.0 0.0 1.0 0.0
* 9 0.0 0.0 0.0 .001 0.0
* 10 0.0 0.0 0.0 1000.0 0.0
* 11 0.0 0.0 0.0 1.0 0.0
* 12 -1.698 -0.0322 0.0 1000.0 0.0
* 13 -.9 0.0 0.0 1000.0 0.0
* 14 0.0 0.0 0.0 1000.0 0.0
* 15 0.0 0.0 0.0 1000.0 0.0
* 16 0.0 0.0 0.0 100.0 0.0
* 17 0.0 0.0 0.0 20.0 0.0
* 18 -0.6 0.0 0.0 100.0 0.0
* 19 0.7 0.0 0.0 20.0 0.0
* 20 0.0 0.0 0.0 1.0 0.0
* 21 0.1 0.0 0.0 1.0 0.0
* 22 0.0 -1.0 0.0 20. 0.0
#
0.01 1. 0.1
#
1 2 3 4 13 15 21
#
1 2 3 4 22 8
0.0 -100.0 20.0 0.0
10. 1.
Distance Height
Seat_Ejection
Delta-Y
Theta
Velocity
Plane-Y
Logical(t>4)
#
1 0.0 0.6 0.6 0.6 0.6
.1 .1154 .1308 .1464 .1612
.177 .1921 .2078 .2232 .2386
.254 .2692 .285 .3 .2 .2
#
