Aviation Ordnanceman Chapter 3 Air-Launched Guided Missiles And Launchers

Front 1

WHAT ARE THE PHYSICAL CHARACTERISTICS OF THE AIM-120 AMRAAM GUIDED MISSILE

Back 1

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

Front 2

WHAT ARE THE TECHNICAL CHARACTERISTICS OF THE LAU-115/A

Back 2

THE TECHNICAL CHARACTERISTICS ARE
WEIGHT:52 POUNDS

HEIGHT:7 INCHES

WIDTH:7 INCHES

LENGTH:78 INCHES

Front 3

WHAT ARE THE TECHNICAL CHARACTERISITCS OF THE LAU-115A/A

Back 3

THE TECHNICAL CHARACTERISTIC
ARE
WEIGHT:59 POUNDS

HEIGHT:7 INCHES

WIDTH:7 INCHES

LENGTH:82 INCHES

Front 4

WHAT ARE THE TECHNICAL CHARACTERISITS OF THE LAU-115B/A

Back 4

THE TECHNICAL CHARACTERISTIC ARE
WEIGHT:59 POUNDS

HEIGHT:7 INCHES

WIDTH: 7 INCHES

LENGTH:82 INCHES

Front 5

WHAT ARE THE TECHNICAL CHARACTERISITS OF THE LAU-115C/A

Back 5

THE TECHNICAL CHARACTERISTIC ARE
WEIGHT:120 POUNDS

HEIGHT:10INCHES

WIDTH:7INCHES

LENGTH:82INCHES

Front 6

WHAT ARE THE PHYSICAL CHARACTERISTICS OF THE LAU-116/A GUIDED MISSILE LAUNCHER

Back 6

THE PHYSICAL CHARACTERISTICS ARE
WEIGHT:65LB

LENGTH:44IN.

WIDTH:9.5IN.

HEIGHT: 16IN.

Front 7

WHAT ARE THE PHYSICAL CHARACTERISTICS OF THE LAU-117/A GUIDED MISSILE LAUNCHER

Back 7

THE PHYSICAL CHARACTERISTICS ARE
WEIGHT:135LB.

LENGTH:93.5IN.

WIDTH:11.0IN.

HEIGHT:9.75IN.

Front 8

WHAT ARE THE PHYSICAL CHARACTERISTICS OF THE LAU-118 GUIDED MISSILE LAUNCHER

Back 8

THE PHYSICAL CHARACTERISTICS ARE
WEIGHT:65LB.

LENGTH:44IN.

WIDTH:9.5 IN.

HEIGHT:16IN.

Front 9

WHAT ARE THE PHYSICAL CHARACTERISTICS OF THE ADU-299/E MISSILE LAUNCHER ADAPTER

Back 9

THE PHYSICAL CHARACTERISTICS ARE
WEIGHT:13LB.

HEIGHT:3 3/4IN.

WIDTH:11IN.

LENGTH:45 1/4 IN.

SUSPENSION: 14 OR 30 IN.

Front 10

WHAT ARE THE PHYSICAL CHARACTERISTICS OF THE LAU-127 GUIDED MISSILE LAUNCHER

Back 10

THE PHYSICAL CHARACTISTICS ARE
WEIGHT:87LB.

LENGTH:115 IN.

WEIGHT:7IN.

HEIGHT:6IN.

Front 11

WITHIN THE RADOM OF THE SPARROW 3 MISSILE, WHAT FEATURE RECEIVES AND INTERPRETS THE RADAR ENERGY REFLECTED FROM THE TARGET

Back 11

WITHIN THE RADOM OF THE SPARROW 3 MISSILE,THE TARGET SEEKER RECEIVES AND INTERPRETS THE RADAR ENERGY REFLECTED FROM THE TARGET

Front 12

WHAT PART OF THE SPARROW 3 MISSILE PRVIDES CONTROL SIGNALS AND MECHANICAL ENERGY TO MOVE EXTERNAL CONTROL SURFACES THAT GUIDE THE MISSILE?

Back 12

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

Front 13

TO WHAT PART OF THE SPARROW MISSILE IS THE DUAL THRUST ROCKET MOTOR(DRTM) ATTACHED

Back 13

THE DUAL THRUST ROCKET MOTOR(DRTM) IS ATTACHED TO THE AFT END OF THE MISSILE FLIGHT CONTROL SECTION OF THE SPARROW MISSILE

Front 14

NAME THE AIRCRAFT FROM WHICH THE HARPOON GUIDED MISSILE IS LAUNCHED

Back 14

THE HARPOON GUIDED MISSILE IS LAUNCHED FROM F/A-18,S3,ANDP-3 AIRCRAFT

Front 15

THE HARPOON MISSILE IS LESS SUSCEPTIBLE TO RADAR DETECTION BECAUSE?

Back 15

THE HARPOON MISSILE IS LESS SUSCEPTIBLE TO RADAR DETECTION BECAUSE OF ITS LOW-LEVEL CRUISE TRAJECTORY WITH OVER-THE-HORIZON RANGE

Front 16

LIST THE SECTIONS OF THE HARPOON MISSILE.

Back 16

THE SECTIONS OF THE HARPOON MISSILE INCLUDE:
THE GUIDANCE,WAR-HEAD,SUSTAINER,AND BOAT-TAIL SECTIONS.

Front 17

SIDEWINDER MISSILES ARE EQUIPPED WITH ? TARGET DETECTION.

Back 17

SIDEWINDER MISSILE ARE EQUIPPED WITH PASSIVE INFRARED TARGET DETECTION.

Front 18

LIST THE FIVE MAJOR COMPONENTS OF THE SIDEWINDER MISSILE.

Back 18

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.

Front 19

BY WHAT MEANS IS THE SAFE&ARM (S&A) DEVICE ALIGNED?

Back 19

AN INTERRUPTED FIRING TRAIN THAT IS ALIGNED BY AN ACCELERATION-ARMING DEVICE ALIGNS THE SAFE & ARM (S&A) DEVICE

Front 20

WHAT FEATURE OF THE SIDEWINDER MISSILE PROVIDES AERODYNAMIC LIFT AND STABILITY DURING FLIGHT?

Back 20

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.

Front 21

LIST THE HOMING CAPABILITIES INCORPORATED INTO THE PHOENIX MISSILE.

Back 21

THE PHOENIX MISSILE USE :ACTIVE,SEMIACTIVE,AND PASSIVE HOMING

Front 22

HOW MANY PHOENIX MISSILES CAN BE LAUNCHED FROM A SIGLE AIRCRAFT?

Back 22

SIX PHOENIX MISSILES CAN BE LAUNCHED FROM A SINGLE AIRCRAFT.

Front 23

LIST THE SECTIONS OF THE PHOENIX MISSILE

Back 23

THE PHOENIX MISSILE CONSISTS OF THE :GUIDANCE,ARMAMENT,PROPULSION,AND CONTROL SECTIONS

Front 24

LIST THE TYPES OF TARGETS THE MAVERICK MISSILE IS USED AGAINST

Back 24

THE MAVERICK MISSILE IS USED AGAINST FORTIFIED GROUND INSTALLATIONS,ARMORED VEHICLES,ANDSURFACE COMBATANTS.

Front 25

HOW DOES THE LASER GUIDANCE SYSTEM WORK IN THE MAVERICK

Back 25

THE MAVERICK MISSILE HAS AUTOMATIC TERMIAL HOMING ON LASER ENERGY REFLECTED FROM THE TARGET,WHICH HAS BEEN ILLUMINATED BY A LASER DESIGNATOR.

Front 26

NAME THE THREE BASIC MODES OF HARM MISSILE OPERATION.

Back 26

THE THREE BASIC MODES OF HARM MISSILE OPERATION ARE:SELF-PROTECT,TARGET OF OPPORTUNITY,AND PREBRIEF.

Front 27

NAME THE FOUR BASIC SERIES OF WALLEYE GUIDED WEAPON SYSTEMS.

Back 27

WALLEYE GUIDED WEAPON SYSTEMS ARE THE WALL 1,WALLEYE 1 EDRL, WALLEYE 2, AND WALL 2 ERDL

Front 28

LIST THE SECTIONS OF THE WALLEYE 1 TACTICAL WEAPON

Back 28

THE SECTIONS OF THE WALLEYE 1 TACTICAL WEAPON INCLUDE THE: GUIDANCE SECTION,WARHEAD SECTION,CONTROL SECTION,FOUR WINGS,AND FOUR FINS

Front 29

WHEN THE WALLEYE 1 IS USED,HOW IS A TYPICAL ATTACK SITUATION FORMED?

Back 29

WHEN THE WALLEYE 1 IS USED,A TYPICAL ATTACK SITUATION IS FORMED BY THE WEAPON,PILOT,ANDAIRCRAFT PERFORMING AS A COMPLETE WEAPONS SYSTEMS.

Front 30

WHAT TYPE OF SUSPENSION DOES THE WALLEYE 2 HAVE?

Back 30

THE WALLEYE 1 AND WALL 2 WEAPONS ARE BASICALLY THE SAME: HOWEVER, THE WALLEYE 2 IS PHYSICALLY LARGER AND HAS IMPROVED ELECTRONICS.

Front 31

WHAT IS THE DIFFERENCE BETWEEN THE WALLEYE 1 AND WALLEYE 2 WEAPONS?

Back 31

THE WALLEYE 2 ERDL HAS ADDED DATA LINK FUNCTIONS AND EXTENDED RANGE CAPABILITY.

Front 32

NAME THE FUNCTIONS OF THE WALLEYE 2 ERDL HAVE THAT THE WALLEYE 1 AND WALLEYE 2 DON'T HAVE

Back 32

THE DATA-LINK POD PROVIDES THE COMMUNICATIONS LINK BETWEEN THE PILOT AND WEAPON

Front 33

THE DATA-LINK POD PROVIDES THE ?

Back 33

THE DATA-LINK POD PROVIDES THE COMMUNICATIONS LINK BETWEEN THE PILOT AND WEAPON

Front 34

WHAT PREVENTS THE CONTROL SECTION OF ONE WEAPON FROM RESPONDING TO COMMANDS NOT SET TO ITS CHANNEL

Back 34

THREE FREQUENCY CHANNELS(A,C,AND E) PREVENT THE CONTROL SECTION OF ONE WEAPON FROM RESPONDING TO COMMANDS NOT SET TO ITS CHANNEL

Front 35

WHAT MISSILE LAUNCHER IS USED TO CARRY AND LAUNCH THE SIDEWINDER MISSILE?

Back 35

THE LAU-7/A MISSILE LAUNCHER IS USED TO CARRY AND LAUNCH THE SIDEWINDER MISSILE

Front 36

LIST THE FOUR MAJOR ASSEMBLIES OF THE LAU-7/A LAUNCHER

Back 36

THE FOUR MAJOR ASSEMBLIES OF THE LAU-7/A LAUNCHER INCLUDE THE : HOUSING,NITROGEN RECEIVER,MECHANISM,AND POWER SUPPLY ASSEMBLIES.

Front 37

WHAT IS THE PURPOSE OF THE NITROGEN RECEIVER ASSEMBLY

Back 37

THE NITROGEN RECEIVER ASSEMBLY IS USED TO STORE HIGH-PRESSURE NITROGEN(3,200PSIG) THAT IS USED TO COOL MISSILE IR DETECTOR GUIDANCE SYSTEMS.

Front 38

WHAT IS THE PURPOSE OF THE DETENT,DETENT LOCK,DETENT-LOCK SOLENOID,AND SNUBBER SUBASSEMBLIES OF THE MECHANISM ASSEMBLY?

Back 38

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.

Front 39

WHAT DOES THE LAU-7/A GUIDED MISSILE LAUNCHER PROVIDE?

Back 39

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.

Front 40

WHAT MISSILE LAUNCHER IS USED TO CARRY AN AIM-7 SPARROW MISSILE ON THE OUTBOARD PYLON OF AN F/A-18 AIRCRAFT

Back 40

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

Front 41

WHAT GUIDED MISSILE LAUNCHER COMPLETES THE F/A-18 AIRCRAFT SUSPENSION AND LAUNCHING SYSTEM FOR THE MAVERICK MISSILE

Back 41

THE LAU-117/A GUIDED MISSILE LAUNCHER COMPLETES THE F/A-18 AIRCRAFT SUSPENSION AND LAUNCHING SYSTEM FOR THE MAVERICK MISSILE

Front 42

WHAT MISSILE IS COMPATIBLE WITH THE LAU-118/A GUIDED MISSILE LAUNCHER

Back 42

THE AGM-88 HARM MISSILE IS COMPATIBLE WITH THE LAU-118/A GUIDED MISSILE LAUNCHER.

Front 43

WHAT CONCEPT SIMPLIFIED THE HANDLING OF GUIDED MISSILES AT THE USER LEVEL

Back 43

THE HANDLING OF GUIDED MISSILES AT THE USERS LEVEL WAS SIMPLIFIED BY THE INTRODUCTION OF THE ALL-UP-ROUND (AUR) CONCEPT

Front 44

THE RESPONSIBILITY FOR ASSEMBLING INDIVIDUAL MISSILE COMPONENTS INTO COMPLETE READY FOR ISSUE (RFI) MISSILE RESTS WITH ?

Back 44

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).

Front 45

WHAT IS THE PURPOSE OF A NAVAL AIR WEAPONS MAINTENANCE UNIT(NAWMU)

Back 45

THE PURPOSE OF A NAVAL AIR WEAPONS MAINTENANCE UNIT(NAWMU) IS TO UPGRADE MISSILES FROM A NON-RFI TO AN RFI STATUS.

Front 46

WHAT SOLUTION IS USED TO LEAK TEST GAS CONTAINERS

Back 46

A SOAPY WATER SOLUTION IS USED TO LEAK TEST GAS CONTAINERS.

Front 47

WHEN HANDLING FORWARD-FIRING ORDNANCE,WHAT IS THE DESIRED PLACE YOU SHOULD WORK.

Back 47

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.