C3, TM9-2350-230-12
1. NULL METER. INDICATES ALIGNMENT OF TRACKER DURING
9. GO LAMP (GREEN). INDICATES OPERATIONAL CONDITION
TRACKER ALIGNMENT TEST AND OPERATIONAL CONDITION
OF GUIDANCE AND CONTROL SYSTEM DURING SELF TEST.
OF RATE SENSOR DURING SYSTEM SELF TEST
10. DIMMER CONTROL. ADJUSTS THE BRIGHTNESS OF ALL
2. XMTR LAMP (RED). INDICATES OPERATIONAL CONDITION
LAMPS EXCEPT THE RED NO/GO LAMPS.
11. RESET SWITCH. TURNS OFF ALL CONTROL SIGNALS. USED
3. CHECKOUT PANEL LAMP (RED). INDICATES OPERATIONAL
DURING TRACKER ALIGNMENT TEST, SYSTEM SELF TEST,
AND TRANSMITTER TEST.
CONDITION OF THE TEST CHECKOUT PANEL DURING
12. LAMP AND METER TEST SWITCH. INITIATES THE TEST OF
SYSTEM SELF TEST.
4. TRACKER
LAMP
(RED).
INDICATES
OPERATIONAL
ALL LAMPS AND THE NULL METER ON THE TEST CHECKOUT
PANEL.
CONDITION OF THE TRACKER DURING SYSTEM SELF TEST.
13. XMTR TEST SWITCH AND LAMP (WHITE). SWITCH TURNS ON
5. POWER SUPPLY LAMP (RED). INDICATES OPERATIONAL
CONDITION OF THE POWER SUPPLY DURING SYSTEM
OPERATION.
14. TRACKER ALIGN SWITCH AND LAMP (WHITE). INITIATES THE
6. SIG DATA CONV LAMP (RED). INDICATES OPERATIONAL
ALIGNMENT TEST OF THE TRACKER.
15. SYSTEM TEST SWITCH AND LAMP (WHITE). INITIATES THE
CONDITION OF THE SIGNAL DATA CONVERTER DURING
SYSTEM SELF TEST.
SYSTEM SELF TEST.
7. PRIME VOLTAGE LAMP (AMBER). IF LAMP GLOWS AFTER
16. AZ/EL SWITCH AND LAMPS (WHITE). SELECTS AZIMUTH AND
SYSTEM WARM-UP THE VEHICLE POWER TO THE SYSTEM
ELEVATION SIGNALS FROM THE RATE SENSOR FOR TEST.
IS LOW.
IT IS ALSO USED DURING THE ALIGNMENT TEST OF THE
8. MOD LAMP (RED). INDICATES OPERATIONAL CONDITION OF
TRACKER TO INDICATE AZIMUTH AND ELEVATION
ALIGNMENT.
THE MODULATOR DURING SYSTEM SELF TEST.
WE 10908B
Figure 2-31. (Superseded) Missile subsystem test checkout panel
2-52