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47 Cards in this Set

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WHAT ARE THE PHYSICAL CHARACTERISTICS OF THE AIM-120 AMRAAM GUIDED MISSILE
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
WHAT ARE THE TECHNICAL CHARACTERISTICS OF THE LAU-115/A
THE TECHNICAL CHARACTERISTICS ARE
WEIGHT:52 POUNDS

HEIGHT:7 INCHES

WIDTH:7 INCHES

LENGTH:78 INCHES
WHAT ARE THE TECHNICAL CHARACTERISITCS OF THE LAU-115A/A
THE TECHNICAL CHARACTERISTIC
ARE
WEIGHT:59 POUNDS

HEIGHT:7 INCHES

WIDTH:7 INCHES

LENGTH:82 INCHES
WHAT ARE THE TECHNICAL CHARACTERISITS OF THE LAU-115B/A
THE TECHNICAL CHARACTERISTIC ARE
WEIGHT:59 POUNDS

HEIGHT:7 INCHES

WIDTH: 7 INCHES

LENGTH:82 INCHES
WHAT ARE THE TECHNICAL CHARACTERISITS OF THE LAU-115C/A
THE TECHNICAL CHARACTERISTIC ARE
WEIGHT:120 POUNDS

HEIGHT:10INCHES

WIDTH:7INCHES

LENGTH:82INCHES
WHAT ARE THE PHYSICAL CHARACTERISTICS OF THE LAU-116/A GUIDED MISSILE LAUNCHER
THE PHYSICAL CHARACTERISTICS ARE
WEIGHT:65LB

LENGTH:44IN.

WIDTH:9.5IN.

HEIGHT: 16IN.
WHAT ARE THE PHYSICAL CHARACTERISTICS OF THE LAU-117/A GUIDED MISSILE LAUNCHER
THE PHYSICAL CHARACTERISTICS ARE
WEIGHT:135LB.

LENGTH:93.5IN.

WIDTH:11.0IN.

HEIGHT:9.75IN.
WHAT ARE THE PHYSICAL CHARACTERISTICS OF THE LAU-118 GUIDED MISSILE LAUNCHER
THE PHYSICAL CHARACTERISTICS ARE
WEIGHT:65LB.

LENGTH:44IN.

WIDTH:9.5 IN.

HEIGHT:16IN.
WHAT ARE THE PHYSICAL CHARACTERISTICS OF THE ADU-299/E MISSILE LAUNCHER ADAPTER
THE PHYSICAL CHARACTERISTICS ARE
WEIGHT:13LB.

HEIGHT:3 3/4IN.

WIDTH:11IN.

LENGTH:45 1/4 IN.

SUSPENSION: 14 OR 30 IN.
WHAT ARE THE PHYSICAL CHARACTERISTICS OF THE LAU-127 GUIDED MISSILE LAUNCHER
THE PHYSICAL CHARACTISTICS ARE
WEIGHT:87LB.

LENGTH:115 IN.

WEIGHT:7IN.

HEIGHT:6IN.
WITHIN THE RADOM OF THE SPARROW 3 MISSILE, WHAT FEATURE RECEIVES AND INTERPRETS THE RADAR ENERGY REFLECTED FROM THE TARGET
WITHIN THE RADOM OF THE SPARROW 3 MISSILE,THE TARGET SEEKER RECEIVES AND INTERPRETS THE RADAR ENERGY REFLECTED FROM THE TARGET
WHAT PART OF THE SPARROW 3 MISSILE PRVIDES CONTROL SIGNALS AND MECHANICAL ENERGY TO MOVE EXTERNAL CONTROL SURFACES THAT GUIDE THE MISSILE?
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
TO WHAT PART OF THE SPARROW MISSILE IS THE DUAL THRUST ROCKET MOTOR(DRTM) ATTACHED
THE DUAL THRUST ROCKET MOTOR(DRTM) IS ATTACHED TO THE AFT END OF THE MISSILE FLIGHT CONTROL SECTION OF THE SPARROW MISSILE
NAME THE AIRCRAFT FROM WHICH THE HARPOON GUIDED MISSILE IS LAUNCHED
THE HARPOON GUIDED MISSILE IS LAUNCHED FROM F/A-18,S3,ANDP-3 AIRCRAFT
THE HARPOON MISSILE IS LESS SUSCEPTIBLE TO RADAR DETECTION BECAUSE?
THE HARPOON MISSILE IS LESS SUSCEPTIBLE TO RADAR DETECTION BECAUSE OF ITS LOW-LEVEL CRUISE TRAJECTORY WITH OVER-THE-HORIZON RANGE
LIST THE SECTIONS OF THE HARPOON MISSILE.
THE SECTIONS OF THE HARPOON MISSILE INCLUDE:
THE GUIDANCE,WAR-HEAD,SUSTAINER,AND BOAT-TAIL SECTIONS.
SIDEWINDER MISSILES ARE EQUIPPED WITH ? TARGET DETECTION.
SIDEWINDER MISSILE ARE EQUIPPED WITH PASSIVE INFRARED TARGET DETECTION.
LIST THE FIVE MAJOR COMPONENTS OF THE SIDEWINDER MISSILE.
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.
BY WHAT MEANS IS THE SAFE&ARM (S&A) DEVICE ALIGNED?
AN INTERRUPTED FIRING TRAIN THAT IS ALIGNED BY AN ACCELERATION-ARMING DEVICE ALIGNS THE SAFE & ARM (S&A) DEVICE
WHAT FEATURE OF THE SIDEWINDER MISSILE PROVIDES AERODYNAMIC LIFT AND STABILITY DURING FLIGHT?
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.
LIST THE HOMING CAPABILITIES INCORPORATED INTO THE PHOENIX MISSILE.
THE PHOENIX MISSILE USE :ACTIVE,SEMIACTIVE,AND PASSIVE HOMING
HOW MANY PHOENIX MISSILES CAN BE LAUNCHED FROM A SIGLE AIRCRAFT?
SIX PHOENIX MISSILES CAN BE LAUNCHED FROM A SINGLE AIRCRAFT.
LIST THE SECTIONS OF THE PHOENIX MISSILE
THE PHOENIX MISSILE CONSISTS OF THE :GUIDANCE,ARMAMENT,PROPULSION,AND CONTROL SECTIONS
LIST THE TYPES OF TARGETS THE MAVERICK MISSILE IS USED AGAINST
THE MAVERICK MISSILE IS USED AGAINST FORTIFIED GROUND INSTALLATIONS,ARMORED VEHICLES,ANDSURFACE COMBATANTS.
HOW DOES THE LASER GUIDANCE SYSTEM WORK IN THE MAVERICK
THE MAVERICK MISSILE HAS AUTOMATIC TERMIAL HOMING ON LASER ENERGY REFLECTED FROM THE TARGET,WHICH HAS BEEN ILLUMINATED BY A LASER DESIGNATOR.
NAME THE THREE BASIC MODES OF HARM MISSILE OPERATION.
THE THREE BASIC MODES OF HARM MISSILE OPERATION ARE:SELF-PROTECT,TARGET OF OPPORTUNITY,AND PREBRIEF.
NAME THE FOUR BASIC SERIES OF WALLEYE GUIDED WEAPON SYSTEMS.
WALLEYE GUIDED WEAPON SYSTEMS ARE THE WALL 1,WALLEYE 1 EDRL, WALLEYE 2, AND WALL 2 ERDL
LIST THE SECTIONS OF THE WALLEYE 1 TACTICAL WEAPON
THE SECTIONS OF THE WALLEYE 1 TACTICAL WEAPON INCLUDE THE: GUIDANCE SECTION,WARHEAD SECTION,CONTROL SECTION,FOUR WINGS,AND FOUR FINS
WHEN THE WALLEYE 1 IS USED,HOW IS A TYPICAL ATTACK SITUATION FORMED?
WHEN THE WALLEYE 1 IS USED,A TYPICAL ATTACK SITUATION IS FORMED BY THE WEAPON,PILOT,ANDAIRCRAFT PERFORMING AS A COMPLETE WEAPONS SYSTEMS.
WHAT TYPE OF SUSPENSION DOES THE WALLEYE 2 HAVE?
THE WALLEYE 1 AND WALL 2 WEAPONS ARE BASICALLY THE SAME: HOWEVER, THE WALLEYE 2 IS PHYSICALLY LARGER AND HAS IMPROVED ELECTRONICS.
WHAT IS THE DIFFERENCE BETWEEN THE WALLEYE 1 AND WALLEYE 2 WEAPONS?
THE WALLEYE 2 ERDL HAS ADDED DATA LINK FUNCTIONS AND EXTENDED RANGE CAPABILITY.
NAME THE FUNCTIONS OF THE WALLEYE 2 ERDL HAVE THAT THE WALLEYE 1 AND WALLEYE 2 DON'T HAVE
THE DATA-LINK POD PROVIDES THE COMMUNICATIONS LINK BETWEEN THE PILOT AND WEAPON
THE DATA-LINK POD PROVIDES THE ?
THE DATA-LINK POD PROVIDES THE COMMUNICATIONS LINK BETWEEN THE PILOT AND WEAPON
WHAT PREVENTS THE CONTROL SECTION OF ONE WEAPON FROM RESPONDING TO COMMANDS NOT SET TO ITS CHANNEL
THREE FREQUENCY CHANNELS(A,C,AND E) PREVENT THE CONTROL SECTION OF ONE WEAPON FROM RESPONDING TO COMMANDS NOT SET TO ITS CHANNEL
WHAT MISSILE LAUNCHER IS USED TO CARRY AND LAUNCH THE SIDEWINDER MISSILE?
THE LAU-7/A MISSILE LAUNCHER IS USED TO CARRY AND LAUNCH THE SIDEWINDER MISSILE
LIST THE FOUR MAJOR ASSEMBLIES OF THE LAU-7/A LAUNCHER
THE FOUR MAJOR ASSEMBLIES OF THE LAU-7/A LAUNCHER INCLUDE THE : HOUSING,NITROGEN RECEIVER,MECHANISM,AND POWER SUPPLY ASSEMBLIES.
WHAT IS THE PURPOSE OF THE NITROGEN RECEIVER ASSEMBLY
THE NITROGEN RECEIVER ASSEMBLY IS USED TO STORE HIGH-PRESSURE NITROGEN(3,200PSIG) THAT IS USED TO COOL MISSILE IR DETECTOR GUIDANCE SYSTEMS.
WHAT IS THE PURPOSE OF THE DETENT,DETENT LOCK,DETENT-LOCK SOLENOID,AND SNUBBER SUBASSEMBLIES OF THE MECHANISM ASSEMBLY?
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.
WHAT DOES THE LAU-7/A GUIDED MISSILE LAUNCHER PROVIDE?
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.
WHAT MISSILE LAUNCHER IS USED TO CARRY AN AIM-7 SPARROW MISSILE ON THE OUTBOARD PYLON OF AN F/A-18 AIRCRAFT
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
WHAT GUIDED MISSILE LAUNCHER COMPLETES THE F/A-18 AIRCRAFT SUSPENSION AND LAUNCHING SYSTEM FOR THE MAVERICK MISSILE
THE LAU-117/A GUIDED MISSILE LAUNCHER COMPLETES THE F/A-18 AIRCRAFT SUSPENSION AND LAUNCHING SYSTEM FOR THE MAVERICK MISSILE
WHAT MISSILE IS COMPATIBLE WITH THE LAU-118/A GUIDED MISSILE LAUNCHER
THE AGM-88 HARM MISSILE IS COMPATIBLE WITH THE LAU-118/A GUIDED MISSILE LAUNCHER.
WHAT CONCEPT SIMPLIFIED THE HANDLING OF GUIDED MISSILES AT THE USER LEVEL
THE HANDLING OF GUIDED MISSILES AT THE USERS LEVEL WAS SIMPLIFIED BY THE INTRODUCTION OF THE ALL-UP-ROUND (AUR) CONCEPT
THE RESPONSIBILITY FOR ASSEMBLING INDIVIDUAL MISSILE COMPONENTS INTO COMPLETE READY FOR ISSUE (RFI) MISSILE RESTS WITH ?
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).
WHAT IS THE PURPOSE OF A NAVAL AIR WEAPONS MAINTENANCE UNIT(NAWMU)
THE PURPOSE OF A NAVAL AIR WEAPONS MAINTENANCE UNIT(NAWMU) IS TO UPGRADE MISSILES FROM A NON-RFI TO AN RFI STATUS.
WHAT SOLUTION IS USED TO LEAK TEST GAS CONTAINERS
A SOAPY WATER SOLUTION IS USED TO LEAK TEST GAS CONTAINERS.
WHEN HANDLING FORWARD-FIRING ORDNANCE,WHAT IS THE DESIRED PLACE YOU SHOULD WORK.
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.