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47 Cards in this Set
- Front
- Back
WHAT ARE THE PHYSICAL CHARACTERISTICS OF THE AIM-120 AMRAAM GUIDED MISSILE
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THE PHYSICAL CHARACTISTIC ARE IN
WEIGHT:327LB. DIMENSIONS:144IN. LENGTH:144IN. DIAMETER:7IN. WING SPAN:21IN. FIN SPAN 25IN. SUSPENSION:LAU-127A/A OR LAU-116A/A |
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WHAT ARE THE TECHNICAL CHARACTERISTICS OF THE LAU-115/A
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THE TECHNICAL CHARACTERISTICS ARE
WEIGHT:52 POUNDS HEIGHT:7 INCHES WIDTH:7 INCHES LENGTH:78 INCHES |
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WHAT ARE THE TECHNICAL CHARACTERISITCS OF THE LAU-115A/A
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THE TECHNICAL CHARACTERISTIC
ARE WEIGHT:59 POUNDS HEIGHT:7 INCHES WIDTH:7 INCHES LENGTH:82 INCHES |
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WHAT ARE THE TECHNICAL CHARACTERISITS OF THE LAU-115B/A
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THE TECHNICAL CHARACTERISTIC ARE
WEIGHT:59 POUNDS HEIGHT:7 INCHES WIDTH: 7 INCHES LENGTH:82 INCHES |
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WHAT ARE THE TECHNICAL CHARACTERISITS OF THE LAU-115C/A
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THE TECHNICAL CHARACTERISTIC ARE
WEIGHT:120 POUNDS HEIGHT:10INCHES WIDTH:7INCHES LENGTH:82INCHES |
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WHAT ARE THE PHYSICAL CHARACTERISTICS OF THE LAU-116/A GUIDED MISSILE LAUNCHER
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THE PHYSICAL CHARACTERISTICS ARE
WEIGHT:65LB LENGTH:44IN. WIDTH:9.5IN. HEIGHT: 16IN. |
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WHAT ARE THE PHYSICAL CHARACTERISTICS OF THE LAU-117/A GUIDED MISSILE LAUNCHER
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THE PHYSICAL CHARACTERISTICS ARE
WEIGHT:135LB. LENGTH:93.5IN. WIDTH:11.0IN. HEIGHT:9.75IN. |
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WHAT ARE THE PHYSICAL CHARACTERISTICS OF THE LAU-118 GUIDED MISSILE LAUNCHER
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THE PHYSICAL CHARACTERISTICS ARE
WEIGHT:65LB. LENGTH:44IN. WIDTH:9.5 IN. HEIGHT:16IN. |
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WHAT ARE THE PHYSICAL CHARACTERISTICS OF THE ADU-299/E MISSILE LAUNCHER ADAPTER
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THE PHYSICAL CHARACTERISTICS ARE
WEIGHT:13LB. HEIGHT:3 3/4IN. WIDTH:11IN. LENGTH:45 1/4 IN. SUSPENSION: 14 OR 30 IN. |
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WHAT ARE THE PHYSICAL CHARACTERISTICS OF THE LAU-127 GUIDED MISSILE LAUNCHER
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THE PHYSICAL CHARACTISTICS ARE
WEIGHT:87LB. LENGTH:115 IN. WEIGHT:7IN. HEIGHT:6IN. |
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WITHIN THE RADOM OF THE SPARROW 3 MISSILE, WHAT FEATURE RECEIVES AND INTERPRETS THE RADAR ENERGY REFLECTED FROM THE TARGET
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WITHIN THE RADOM OF THE SPARROW 3 MISSILE,THE TARGET SEEKER RECEIVES AND INTERPRETS THE RADAR ENERGY REFLECTED FROM THE TARGET
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WHAT PART OF THE SPARROW 3 MISSILE PRVIDES CONTROL SIGNALS AND MECHANICAL ENERGY TO MOVE EXTERNAL CONTROL SURFACES THAT GUIDE THE MISSILE?
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THE FLIGHT CONTROL SECTION,WHICH CONSISTS OF THE AUTOPILOT AND HYDRAULIC GROUP,PROVIDES THE SPARROW 3 MISSILE WITH CONTROL SIGLES AND MECHANICAL ENERGY TO MOVE EXTERNAL CONTROL SURFACES TO GUIDE THE MISSILE
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TO WHAT PART OF THE SPARROW MISSILE IS THE DUAL THRUST ROCKET MOTOR(DRTM) ATTACHED
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THE DUAL THRUST ROCKET MOTOR(DRTM) IS ATTACHED TO THE AFT END OF THE MISSILE FLIGHT CONTROL SECTION OF THE SPARROW MISSILE
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NAME THE AIRCRAFT FROM WHICH THE HARPOON GUIDED MISSILE IS LAUNCHED
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THE HARPOON GUIDED MISSILE IS LAUNCHED FROM F/A-18,S3,ANDP-3 AIRCRAFT
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THE HARPOON MISSILE IS LESS SUSCEPTIBLE TO RADAR DETECTION BECAUSE?
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THE HARPOON MISSILE IS LESS SUSCEPTIBLE TO RADAR DETECTION BECAUSE OF ITS LOW-LEVEL CRUISE TRAJECTORY WITH OVER-THE-HORIZON RANGE
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LIST THE SECTIONS OF THE HARPOON MISSILE.
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THE SECTIONS OF THE HARPOON MISSILE INCLUDE:
THE GUIDANCE,WAR-HEAD,SUSTAINER,AND BOAT-TAIL SECTIONS. |
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SIDEWINDER MISSILES ARE EQUIPPED WITH ? TARGET DETECTION.
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SIDEWINDER MISSILE ARE EQUIPPED WITH PASSIVE INFRARED TARGET DETECTION.
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LIST THE FIVE MAJOR COMPONENTS OF THE SIDEWINDER MISSILE.
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THE FIVE MAJOR COMPONENTS OF THE SIDEWINDER MISSILE INCLUDE:THE GUIDANCE AND CONTROL SECTION,TARGET DETECTOR SECTION,S&A DEVICE,WAR-HEAD SECTION,AND ROCKET MOTOR SECTION.
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BY WHAT MEANS IS THE SAFE&ARM (S&A) DEVICE ALIGNED?
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AN INTERRUPTED FIRING TRAIN THAT IS ALIGNED BY AN ACCELERATION-ARMING DEVICE ALIGNS THE SAFE & ARM (S&A) DEVICE
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WHAT FEATURE OF THE SIDEWINDER MISSILE PROVIDES AERODYNAMIC LIFT AND STABILITY DURING FLIGHT?
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FOUR MK 1 MOD 0 OR MOD 1 WINGS ATTACHED TO THE AFT END OF THE MOTOR TUBE PROVIDE AERODYNAMIC LIFT AND STABILITY TO THE SIDEWINDER MISSILE DURING FLIGHT.
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LIST THE HOMING CAPABILITIES INCORPORATED INTO THE PHOENIX MISSILE.
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THE PHOENIX MISSILE USE :ACTIVE,SEMIACTIVE,AND PASSIVE HOMING
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HOW MANY PHOENIX MISSILES CAN BE LAUNCHED FROM A SIGLE AIRCRAFT?
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SIX PHOENIX MISSILES CAN BE LAUNCHED FROM A SINGLE AIRCRAFT.
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LIST THE SECTIONS OF THE PHOENIX MISSILE
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THE PHOENIX MISSILE CONSISTS OF THE :GUIDANCE,ARMAMENT,PROPULSION,AND CONTROL SECTIONS
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LIST THE TYPES OF TARGETS THE MAVERICK MISSILE IS USED AGAINST
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THE MAVERICK MISSILE IS USED AGAINST FORTIFIED GROUND INSTALLATIONS,ARMORED VEHICLES,ANDSURFACE COMBATANTS.
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HOW DOES THE LASER GUIDANCE SYSTEM WORK IN THE MAVERICK
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THE MAVERICK MISSILE HAS AUTOMATIC TERMIAL HOMING ON LASER ENERGY REFLECTED FROM THE TARGET,WHICH HAS BEEN ILLUMINATED BY A LASER DESIGNATOR.
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NAME THE THREE BASIC MODES OF HARM MISSILE OPERATION.
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THE THREE BASIC MODES OF HARM MISSILE OPERATION ARE:SELF-PROTECT,TARGET OF OPPORTUNITY,AND PREBRIEF.
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NAME THE FOUR BASIC SERIES OF WALLEYE GUIDED WEAPON SYSTEMS.
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WALLEYE GUIDED WEAPON SYSTEMS ARE THE WALL 1,WALLEYE 1 EDRL, WALLEYE 2, AND WALL 2 ERDL
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LIST THE SECTIONS OF THE WALLEYE 1 TACTICAL WEAPON
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THE SECTIONS OF THE WALLEYE 1 TACTICAL WEAPON INCLUDE THE: GUIDANCE SECTION,WARHEAD SECTION,CONTROL SECTION,FOUR WINGS,AND FOUR FINS
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WHEN THE WALLEYE 1 IS USED,HOW IS A TYPICAL ATTACK SITUATION FORMED?
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WHEN THE WALLEYE 1 IS USED,A TYPICAL ATTACK SITUATION IS FORMED BY THE WEAPON,PILOT,ANDAIRCRAFT PERFORMING AS A COMPLETE WEAPONS SYSTEMS.
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WHAT TYPE OF SUSPENSION DOES THE WALLEYE 2 HAVE?
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THE WALLEYE 1 AND WALL 2 WEAPONS ARE BASICALLY THE SAME: HOWEVER, THE WALLEYE 2 IS PHYSICALLY LARGER AND HAS IMPROVED ELECTRONICS.
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WHAT IS THE DIFFERENCE BETWEEN THE WALLEYE 1 AND WALLEYE 2 WEAPONS?
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THE WALLEYE 2 ERDL HAS ADDED DATA LINK FUNCTIONS AND EXTENDED RANGE CAPABILITY.
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NAME THE FUNCTIONS OF THE WALLEYE 2 ERDL HAVE THAT THE WALLEYE 1 AND WALLEYE 2 DON'T HAVE
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THE DATA-LINK POD PROVIDES THE COMMUNICATIONS LINK BETWEEN THE PILOT AND WEAPON
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THE DATA-LINK POD PROVIDES THE ?
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THE DATA-LINK POD PROVIDES THE COMMUNICATIONS LINK BETWEEN THE PILOT AND WEAPON
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WHAT PREVENTS THE CONTROL SECTION OF ONE WEAPON FROM RESPONDING TO COMMANDS NOT SET TO ITS CHANNEL
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THREE FREQUENCY CHANNELS(A,C,AND E) PREVENT THE CONTROL SECTION OF ONE WEAPON FROM RESPONDING TO COMMANDS NOT SET TO ITS CHANNEL
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WHAT MISSILE LAUNCHER IS USED TO CARRY AND LAUNCH THE SIDEWINDER MISSILE?
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THE LAU-7/A MISSILE LAUNCHER IS USED TO CARRY AND LAUNCH THE SIDEWINDER MISSILE
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LIST THE FOUR MAJOR ASSEMBLIES OF THE LAU-7/A LAUNCHER
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THE FOUR MAJOR ASSEMBLIES OF THE LAU-7/A LAUNCHER INCLUDE THE : HOUSING,NITROGEN RECEIVER,MECHANISM,AND POWER SUPPLY ASSEMBLIES.
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WHAT IS THE PURPOSE OF THE NITROGEN RECEIVER ASSEMBLY
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THE NITROGEN RECEIVER ASSEMBLY IS USED TO STORE HIGH-PRESSURE NITROGEN(3,200PSIG) THAT IS USED TO COOL MISSILE IR DETECTOR GUIDANCE SYSTEMS.
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WHAT IS THE PURPOSE OF THE DETENT,DETENT LOCK,DETENT-LOCK SOLENOID,AND SNUBBER SUBASSEMBLIES OF THE MECHANISM ASSEMBLY?
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THE DETENT,DETENT LOCK,DETENT-LOCK SOLENOID,AND SNUBBER SUBASSEMBLIES OF THE MECHANISM ASSEMBLY ARE AN ELECTROMECHANICAL SYSTEM THAT RESTRICKS LONGITUDINAL AND LATERAL MOVEMENT OF MOUNTED MISSILE. THIS PREVENTS ACCIDENTAL LAUNCH OR RELEASE DURING CATAPULT TAKE-OFF OR ARRESTED LANDINGS.
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WHAT DOES THE LAU-7/A GUIDED MISSILE LAUNCHER PROVIDE?
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THE LAU-7/A GUIDED MISSILE LAUNCHER PROVIDES A COMPLETE SYSTEM THAT LETS THE PILOT MONITOR THE CONDITION OF THE MISSILE DURING FLIGHT,CONTROL MODE OF OPERATION OF THE MISSILE GUIDANCE SYSTEM, AND INITIATE ARMING AND LAUNCH SEQUENCE.
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WHAT MISSILE LAUNCHER IS USED TO CARRY AN AIM-7 SPARROW MISSILE ON THE OUTBOARD PYLON OF AN F/A-18 AIRCRAFT
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THE LAU-115/A SERIES GUIDED MISSILE LAUNCHER IS USED TO CARRY AN AIM-7 SPARROW MISSILE ON THE OUTBOARD PYLON OF AN F/A-18
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WHAT GUIDED MISSILE LAUNCHER COMPLETES THE F/A-18 AIRCRAFT SUSPENSION AND LAUNCHING SYSTEM FOR THE MAVERICK MISSILE
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THE LAU-117/A GUIDED MISSILE LAUNCHER COMPLETES THE F/A-18 AIRCRAFT SUSPENSION AND LAUNCHING SYSTEM FOR THE MAVERICK MISSILE
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WHAT MISSILE IS COMPATIBLE WITH THE LAU-118/A GUIDED MISSILE LAUNCHER
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THE AGM-88 HARM MISSILE IS COMPATIBLE WITH THE LAU-118/A GUIDED MISSILE LAUNCHER.
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WHAT CONCEPT SIMPLIFIED THE HANDLING OF GUIDED MISSILES AT THE USER LEVEL
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THE HANDLING OF GUIDED MISSILES AT THE USERS LEVEL WAS SIMPLIFIED BY THE INTRODUCTION OF THE ALL-UP-ROUND (AUR) CONCEPT
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THE RESPONSIBILITY FOR ASSEMBLING INDIVIDUAL MISSILE COMPONENTS INTO COMPLETE READY FOR ISSUE (RFI) MISSILE RESTS WITH ?
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THE RESPONSIBILITY FOR ASSEMBLING INDIVIDUAL MISSILE COMPONENTS INTO COMPLETE READY FOR ISSUE(RFI) MISSILES RESTS WITH NAVAL AMMUNTION DEPOT (NAD) OR NAVAL WEAPONS STATION(NWS).
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WHAT IS THE PURPOSE OF A NAVAL AIR WEAPONS MAINTENANCE UNIT(NAWMU)
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THE PURPOSE OF A NAVAL AIR WEAPONS MAINTENANCE UNIT(NAWMU) IS TO UPGRADE MISSILES FROM A NON-RFI TO AN RFI STATUS.
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WHAT SOLUTION IS USED TO LEAK TEST GAS CONTAINERS
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A SOAPY WATER SOLUTION IS USED TO LEAK TEST GAS CONTAINERS.
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WHEN HANDLING FORWARD-FIRING ORDNANCE,WHAT IS THE DESIRED PLACE YOU SHOULD WORK.
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WHEN HANDLING FORWARD-FIRING ORDNANCE,YOU SHOULD WORK ON THE SIDES.WORK IN FRONT OR REAR OF THE ORDNANCE SHOULD BE KEPT TO A MINIMUM.
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