XASM
By Dan Strick on January 27, 2011
1-Rear control surfaces(27 square in.)
2-Solid rocket motor(2.5 sec booster\5 sec sustain)
3-Ignition cap primer
4-H.E warhead(TNT equivalence-36kg)
5-Autopilot with proportional navigational guidance system(13G 3-axis accelerometer)
6-3-axis high sensitive fiber optic gyroscope
7-Front roll\pitch control surfaces(+\- 15 degree)
8-Roll\pitch hydrolic actuators(Solenoid controlled valves)
9-Hydrolic pressurized tank(NO2)
10-Hydrolic pressure connection
11-Infrared\gyro platform signal processor
12-3-axis gyro stabilized infrared seeker(20deg lat\30deg vert)
13-Infrared seeker dome
Click here for self test.. http://www.youtube.com/watch?v=C8Zft5r0EzI
Report
2-Solid rocket motor(2.5 sec booster\5 sec sustain)
3-Ignition cap primer
4-H.E warhead(TNT equivalence-36kg)
5-Autopilot with proportional navigational guidance system(13G 3-axis accelerometer)
6-3-axis high sensitive fiber optic gyroscope
7-Front roll\pitch control surfaces(+\- 15 degree)
8-Roll\pitch hydrolic actuators(Solenoid controlled valves)
9-Hydrolic pressurized tank(NO2)
10-Hydrolic pressure connection
11-Infrared\gyro platform signal processor
12-3-axis gyro stabilized infrared seeker(20deg lat\30deg vert)
13-Infrared seeker dome
Click here for self test.. http://www.youtube.com/watch?v=C8Zft5r0EzI