The missile silo (figure 1-2) is a reinforced, concrete structure with inside dimensions of approximately 146 feet in depth and 55 feet in diameter. Above ground, non-hardened facilities include vehicle parking areas, security fencing and lighting, propellant and electrical connections, static grounding system, commercial power lines, a transformer, cooling tower pits, access portal, non-hardened antennas, soft water storage, area security surveillance system, and weather instruments. Hardened facilities include the missile silo, control center, blast lock, interconnecting cable-ways, emergency escape hatch, and hardened communications equipment. The launch complex includes both above ground and hardened underground facilities. LAUNCH COMPLEX FACILITIES LAUNCH COMPLEX. Squadron maintenance areas provide facilities for supply, administration, operations, and maintenance necessary to maintain the launch complexes in a constant state of readiness. Safety rules for the LGM-25C (Titan II) MK6 RV/MK53 Weapon System (U) are contained in AFR 122-22. All in-commission missiles are maintained in a constant alert condition and may be counted down individually or simultaneously. For maximum safety and effectiveness, individual launch complexes are separated by distance of 7 to 10 nautical miles. The launch complex is designed to maintain an operational readiness condition with no outside support after sustaining an attack that destroys all non-hardened facilities. The weapon system is capable of destroying enemy targets over 5000 nautical miles distant. The LGM-25C Weapon System consists of an inertially guided, liquid fueled, airborne weapon and associated ground equipment necessary to maintain and launch the airborne weapon. This is a manual for the United States Titan II Intercontinental Ballistic Missile weapon system as displayed at the Titan Missile Museum in Sahuarita, Arizona. 47.4 MISSILE SYSTEMS ANALYST TECHNICIAN.47.3 DEPUTY MISSILE COMBAT CREW COMMANDER.47 SECTION VII MISSILE COMBAT CREW DUTIES.44 EMERGENCY EVACUATION OF INJURED PERSONNEL.39.1 ROCKET FUEL HANDLER'S CLOTHING OUTFIT.38 AREA SECURITY SURVEILLANCE EQUIPMENT.37 HAZARD SENSING AND WARNING EQUIPMENT.21.2 INTER-COMPLEX RADIO COMMUNICATION SYSTEM ANTENNAS.21.1 RADIO-TYPE MAINTENANCE NETWORK ANTENNAS.19.3 INTER-COMPLEX RADIO COMMUNICATIONS SYSTEM.19 INTER-COMPLEX COMMUNICATIONS SYSTEM.18.9 RTMN HEADSETS FOR EMERGENCY BREATHING APPARATUS.18 INTRA-COMPLEX COMMUNICATIONS SYSTEM.16.1 MISSILE GUIDANCE ALIGNMENT-CHECKOUT GROUP.15 THRUST MOUNT AND SHOCK ISOLATION SYSTEM.12.5 ELECTRONIC COMMAND SIGNALS PROGRAMMER.12.4 BUTTERFLY VALVE LOCK STATUS DECODER AND DISPLAY.12.3 BUTTERFLY VALVE LOCK STATUS ENCODER.11.1 LAUNCH CONTROL COMPLEX FACILITIES CONSOLE.10.2 NON-PORTABLE MAINTENANCE GROUND EQUIPMENT.10.1 PORTABLE MAINTENANCE GROUND EQUIPMENT.6.6 FIRE WATER CONTROL SWITCH (After MCL 3316).6.5 FIRE WATER RECIRCULATION SYSTEM (After MCL 3315).6.2 FIRE PROTECTION AND PREVENTION SYSTEM.4.3 LAUNCH DUCT AIR CONDITIONING SYSTEM.4.2 ACCESS PORTAL AND BLAST LOCK VENTILATING SYSTEM.4.1 CONTROL CENTER AIR CONDITIONING, HEATING AND VENTILATION SYSTEM.4 AIR CONDITIONING, HEATING, AND VENTILATION SYSTEM.3.5 BLAST LOCK, CABLE-WAYS, AND DECONTAMINATION AREA.
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