AIR LAUNCHED GUIDED MISSILES & GUIDED MISSILE LAUNCHERS

LONG RANGE MISSILES ARE USUALLY CAPABLE OF TRAVELING WHAT MINIMUM NUMBER OF MILES? A. 100 B. 200 C. 300 D. 400

A. 100

WHICH OF THE FOLLOWING DESCRIPTIONS IDENTIFY THE CLASSIFICATIONS OF MISSILE HOMING SYSTEMS? A. ACTIVE, SEMIACTIVE, & PASSIVE B. RADAR, INFRARED, & THERMAL C. SEMIACTIVE, RADAR REFLECTION, & THERMAL D. TARGET ILLUMINATION, INFRARED RAYS, & RADAR

A. ACTIVE, SEMIACTIVE, & PASSIVE

TO REPOSITION THE SAFE ARM ASSEMBLY IN AN AIM-7M GUIDED MISSILE, WHAT TOOL SHOULD BE USED? A. AN ARMING KEY B. A SCREWDRIVER C. A 1/2 INCH WRENCH D. A 1/4 INCH WRENCH

A. AN ARMING KEY

WHAT IS THE BASELINE WEAPON PAYLOAD USED IN THE JSOW AGM-154A? A. BOMB ASSEMBLY SUU-81/B WHICH CONTAINS 145 BLU-97A/B BOMBLETS B. BOMB ASSEMBLY SUU-81/B WHICH CONTAINS A UNITARY SHAPED CHARGE C. ROCKEYE II CBU-99/CBU-100 D. APAM CBU-59/B

A. BOMB ASSEMBLY SUU-81/B WHICH CONTAINS 145 BLU-97A/B BOMBLETS

A GUIDED MISSILE THAT INCORPORATES BOTH A BOOST PHASE & A SUSTAINING THRUST PHASE HAS WHAT DESIGNATION? A. DTRM B. DPRM C. DRM D. DRTS

A. DTRM

AN AIM-9M SIDEWINDER GUIDED MISSILE HAS WHAT NUMBER OF MAJOR COMPONENTS? A. FIVE B. SEVEN C. EIGHT D. NINE

A. FIVE

WHAT TOOL SHOULD BE USED TO REPOSITION THE SAFE ARM IGNITION ASSEMBLY OF A MK 36 MOD 8 ROCKET MOTOR? A. HEX HEAD T HANDLE B. SCREWDRIVER C. ARMING KEY D. ALLEN WRENCH

A. HEX HEAD T HANDLE

SPEEDS ABOVE MACH 5.0 ARE REFERRED TO BY WHAT TERM? A. HYPERSONIC B. SUBSONIC C. SUPERSONIC D. TRANSONIC

A. HYPERSONIC

A MAVERICK MISSILE USES WHAT TYPE OF GUIDANCE SYSTEM? A. LASER B. ACTIVE C. PASSIVE D. COMMAND

A. LASER

WHICH OF THE FOLLOWING GUIDED MISSILE LAUNCHERS, IS A COMPLETE LAUNCHING SYSTEM USED WITH AIM-9 MISSILES? A. LAU-7 B. LAU-9 C. LAU-116 D. LAU-118

A. LAU-7

THE AIM-9X MISSILE INTERFACES WITH THE AIRCRAFT THROUGH THE MISSILE LAUNCHER USING AN UMBILICAL CABLE & WHAT? A. MID BODY BUFFER CONNECTOR B. WIRING HARNESS C. POWER SUPPLY D. HARNESS COVER

A. MID BODY BUFFER CONNECTOR

WHAT SYSTEM COMPRESSES & FILTERS AMBIENT AIR TO GENERATE HIGH PRESSURE PURE AIR USED IN COOLING THE INFRARED DETECTOR IN THE MISSILE GUIDANCE SECTION? A. PURE AIR GENERATING B. NITROGEN C. POWER SUPPLY D. INTERFACE

A. PURE AIR GENERATING

AN AGM-84D GUIDED MISSILE IS DESIGNED TO BE USED AGAINST WHICH OF THE FOLLOWING TARGETS? A. SHIPS B. BUNKERS C. PERSONNEL D. TANKS

A. SHIPS

SPEEDS UP TO MACH 0.8 ARE REFERRED TO BY WHAT TERM? A. SUBSONIC B. TRANSONIC C. SUPERSONIC D. HYPERSONIC

A. SUBSONIC

THE SERIAL NUMBER OF A MISSILE CAN BE FOUND ON WHICH OF THE FOLLOWING MISSILE COMPONENTS? A. THE LEADING COMPONENT B. THE MOTOR C. THE TAIL SECTION D. THE EXPLOSIVE SECTION

A. THE LEADING COMPONENT

WHICH OF THE FOLLOWING PROPULSION SYSTEMS DOES NOT REQUIRE OXYGEN FROM THE ATMOSPHERE FOR ITS OPERATION? A. THERMAL JET B. TURBOJET C. PULSEJET D. RAMJET

A. THERMAL JET

IN AN AIM-7M GUIDED MISSILE, WHAT DEVICE PREVENTS THE MOTOR FROM BEING ACCIDENTALLY FIRED? A. A SAFETY & ARM DEVICE B. A SAFE/ARM IGNITER C. A SHORTING CAP D. A SHORTING PIN

B. A SAFE/ARM IGNITER

WHAT MISSILE USES GUIDANCE PROVIDED THROUGH RECEPTION OF SIGNALS EMITTED FROM GROUND BASED THREAT RADAR & HAS THE CAPABILITY OF DISCRIMINATING A SINGLE TARGET? A. AGM-65 B. AGM-88 C. AGM-114 D. AGM-154

B. AGM-88

TO PREVENT CERTAIN TYPES OF EXERCISE MISSILES FROM TRAVELING BEYOND THE TARGET RANGE, WHAT SAFETY MEASURE SHOULD BE INSTALLED IN THE MISSILES? A. A TRACING FLARE B. AN EXPLOSIVE DESTRUCT CHARGE C. A TELEMETRY TYPE WARHEAD D. A PREPROGRAMMED COMPUTER SYSTEM

B. AN EXPLOSIVE DESTRUCT CHARGE

WHICH OF THE FOLLOWING ITEMS ARE THE MAJOR ASSEMBLIES OF THE LAU-7 GUIDED MISSILE LAUNCHER? A. HOUSING, NITROGEN RECEIVER, POWER SUPPLY, & ELECTRICAL CONVERTER B. HOUSING, MECHANISM, POWER SUPPLY, & NITROGEN RECEIVER C. HOUSING, NITROGEN RECEIVER, & FORWARD FIRING D. HOUSING, MECHANISM, & UMBILICAL HOOK SUPPORT

B. HOUSING, MECHANISM, POWER SUPPLY, & NITROGEN RECEIVER

WHAT LAUNCHERS ARE CAPABLE OF CARRYING & LAUNCHING THE AIM-9X MISSILE? A. LAU-7 & LAU-118 B. LAU-7 & LAU-127 C. LAU-115 & LAU-117 D. LAU-117 & LAU-118

B. LAU-7 & LAU-127

WHICH OF THE FOLLOWING STATEMENTS DESCRIBES AN AIM-7M GUIDED MISSILE? A. AIR TO GROUND MISSILE B. LAUNCHED FROM AN INTERCEPTOR AIRCRAFT C. SURFACE LAUNCHED MISSILE D. TRANSONIC MISSILE

B. LAUNCHED FROM AN INTERCEPTOR AIRCRAFT

A TRAINING MISSILE IS CLASSIFIED AS WHAT TYPE OF MISSILE? A. NONACTIVE B. NONSERVICE C. TACTICAL D. SERVICE

B. NONSERVICE

WHAT TYPE OF GUIDANCE SYSTEM IS USED IN AN AIM-7M GUIDED MISSILE? A. ACTIVE B. SEMIACTIVE C. PASSIVE D. COMMAND

B. SEMIACTIVE

WHAT MISSILE HAS A HIGHLY ACCURATE GPS AIDED GUIDANCE SYSTEM, AN IMAGING INFRARED SEEKER, & A TWO WAY DATA LINK WITH THE AWW-13 ADVANCED DATA LINK POD? A. HARM AGM-88 B. SLAM-ER AGM-84 H/K C. AMRAAM AIM-120 D. JSOW AGM-154

B. SLAM-ER AGM-84 H/K

THE SAFETY & ARMING DEVICE ON A MISSILE IS USED FOR WHAT PURPOSE? A. TO PREVENT ARMING IF THE MISSILE IS FIRED ACCIDENTALLY B. TO MAINTAIN THE EXPLOSIVE TRAIN OF THE FUZING SYSTEM IN A SAFE CONDITION UNTIL CERTAIN REQUIREMENTS ARE MET C. TO PREVENT THE MISSILE FROM BEING ACCIDENTALLY FIRED WHEN THE AIRCRAFT IS NOT AIRBORNE D. TO MAINTAIN THE EXPLOSIVE TRAIN OF THE FUZING SYSTEM IN AN UNSAFE CONDITION BEFORE FIRING THE MISSILE

B. TO MAINTAIN THE EXPLOSIVE TRAIN OF THE FUZING SYSTEM IN A SAFE CONDITION UNTIL CERTAIN REQUIREMENTS ARE MET

WHAT WARHEAD IS USED IN AN AIM-9M GUIDED MISSILE? A. WDU-7/B B. WDU-17/B C. MK 34 D. MK 43

B. WDU-17/B

WHICH OF THE FOLLOWING COLOR CODES ARE USED IN MISSILE IDENTIFICATION? A. YELLOW, BROWN, & BLACK B. YELLOW, BROWN, & BLUE C. BLUE, ORANGE, & RED D. BLUE, ORANGE, & GREEN

B. YELLOW, BROWN, & BLUE

A HIGH EXPLOSIVE WARHEAD USED IN AN AIR TO AIR GUIDED MISSILE CONTAINS WHAT RANGE OF EXPLOSIVES, IN POUNDS? A. 75 TO 100 B. 35 TO 65 C. 10 TO 18 D. 5 TO 10

C. 10 TO 18

WHAT MISSILE IS AN ANTIARMOR TERMINAL HOMING WEAPON THAT USES A VARIETY OF WARHEAD CONFIGURATIONS, INCLUDING SHAPED CHARGE, BLAST FRAGMENTATION, & THERMOBARIC? A. AGM-65 B. AGM-88 C. AGM-114 D. AGM-154

C. AGM-114

THE LAU-127 GUIDED MISSILE LAUNCHER IS DESIGNED TO CARRY & LAUNCH WHAT TYPE OF MISSILE? A. AIM-7 & AIM-9 B. AIM-7 & AIM-120 C. AIM-9 & AIM-120 D. AGM-114 & AIM-120

C. AIM-9 & AIM-120

IN SEMIACTIVE HOMING, TARGET ILLUMINATION COMES FROM WHICH OF THE FOLLOWING SOURCES? A. THE MISSILES GUIDANCE SECTION B. THE MISSILES CONTROL SECTION C. AN EXTERNAL SOURCE TO THE MISSILE D. A RADAR RECEIVER

C. AN EXTERNAL SOURCE TO THE MISSILE

WHAT TWO DISTINCT INTERFACE CONFIGURATIONS ARE USED FOR THE AIM-9X MISSILE? A. DIGITAL & INTERFACE B. ANALOG & ACTIVE C. DIGITAL & ANALOG D. INTERFACE & ACTIVE

C. DIGITAL & ANALOG

WHICH OF THE FOLLOWING MISSILE PROPULSION SYSTEMS IS NOT A THERMAL JET PROPULSION SYSTEM? A. SOLID PROPELLANT B. LIQUID PROPELLANT C. GAS PROPELLANT D. COMBINED PROPELLANT

C. GAS PROPELLANT

WHICH OF THE FOLLOWING MISSILE COMPONENTS IS THE BRAIN OF THE MISSILE? A. NOSE SECTION B. ARMAMENT SECTION C. GUIDANCE SECTION D. PROPULSION SECTION

C. GUIDANCE SECTION

WHAT IS THE AIRCRAFT SUSPENSION & LAUNCHING SYSTEM USED FOR THE AIM-7 SPARROW & AIM-120 AMRAAM MISSILES? A. LAU-7 B. LAU-115 C. LAU-116 D. LAU-117

C. LAU-116

THE DESIGNATION AGM-65E IDENTIFIES WHAT MISSILE? A. HARPOON B. HELLFIRE C. MAVERICK D. SIDEWINDER

C. MAVERICK

WHAT MODIFICATION OF A MK 36 ROCKET MOTOR IS EQUIPPED WITH A SAFE ARM IGNITION ASSEMBLY? A. MOD 6 B. MOD 7 C. MOD 8 D. MOD 9

C. MOD 8

IN THE LAU-7 GUIDED MISSILE LAUNCHER, THE MISSILES INFRARED DETECTOR IS COOLED BY WHAT MEANS? A. RAM AIR TURBINE B. AMBIENT AIR C. NITROGEN RECEIVER D. INDUCTION AIR

C. NITROGEN RECEIVER

WHAT TYPE OF GUIDANCE SYSTEM IS USED IN A SIDEWINDER GUIDED MISSILE? A. PASSIVE B. ACTIVE C. PASSIVE INFRARED D. SEMIACTIVE INFRARED TARGET DETECTION

C. PASSIVE INFRARED

SPEEDS FROM MACH 1.2 TO MACH 5.0 ARE REFERRED TO BY WHAT TERM? A. SUBSONIC B. TRANSONIC C. SUPERSONIC D. HYPERSONIC

C. SUPERSONIC

WHAT SECTION OF A HARPOON MISSILE CONTAINS THE MISSILE BATTERY? A. CONTROL B. GUIDANCE C. SUSTAINER D. WARHEAD

C. SUSTAINER

A SERVICE MISSILE IS USUALLY REFERRED TO AS WHAT TYPE OF MISSILE? A. DUMMY B. PRACTICE C. TACTICAL D. TRAINING

C. TACTICAL

THE CONTROL FINS SHOULD BE ATTACHED TO WHAT SECTION OF A HARPOON MISSILE? A. THE WARHEAD SECTION B. THE SUSTAINER SECTION C. THE CONTROL SECTION D. THE GUIDANCE SECTION

C. THE CONTROL SECTION

AN AGM-88C GUIDED MISSILE IS DESIGNED TO OPERATE IN WHAT TOTAL NUMBER OF MODES? A. ONE B. TWO C. THREE D. FOUR

C. THREE

WHAT PROPULSION SYSTEM IS CURRENTLY BEING USED IN NAVY AIR LAUNCHED MISSILES AS AN ATMOSPHERIC JET PROPULSION SYSTEM? A. PULSEJET B. THERMAL JET C. TURBOJET D. RAMJET

C. TURBOJET

WHAT ARE THE MAJOR DIFFERENCES BETWEEN THE VARIANTS OF THE HELLFIRE MISSILE? A. GUIDANCE SECTION B. CONTROL SECTION C. WARHEAD SECTION D. PROPULSION SECTION

C. WARHEAD SECTION

WHAT TYPE OF GUIDANCE SYSTEM IS USED IN A HARPOON GUIDED MISSILE? A. SEMIACTIVE B. COMMAND C. PASSIVE D. ACTIVE

D. ACTIVE

WHAT WEAPON HAS AN INHERENT RANGE CAPABILITY FOR THE NAVY, AIR FORCE, & MARINE CORPS, THAT SATISFIES THE STAND OFF REQUIREMENTS FOR ATTACKING INTERDICTION TARGETS FROM OUTSIDE ENEMY POINT DEFENSES DURING DAY, NIGHT, & ADVERSE WEATHER CONDITIONS? A. AGM-84K B. AGM 88 C. AGM-114 D. AGM-154

D. AGM-154

WHAT MISSILE DESIGNATOR IS ASSIGNED TO AN AIR LAUNCHED, AERIAL INTERCEPT MISSILE IN THE 9TH DESIGN & THE 13TH MODIFICATION? A. AGM-91 B. AGM-9B C. AIM-9G D. AIM-9M

D. AIM-9M

IN AN AIM-7M GUIDED MISSILE, THE FLIGHT CONTROL SECTION CONSISTS OF WHICH OF THE FOLLOWING COMPONENTS? A. A TARGET SEEKER B. AN AUTOPILOT ONLY C. A HYDRUALIC GROUP ONLY D. AN AUTOPILOT & A HYDRUALIC GROUP

D. AN AUTOPILOT & A HYDRUALIC GROUP

MISSILE PROPULSION SYSTEMS USE WHICH OF THE FOLLOWING BASIC TYPES OF JET POWER PLANTS? A. SOLID PROPELLANT GRAIN ONLY B. LIQUID PROPELLANT MOTOR ONLY C. SOLID PROPELLANT GRAIN & LIQUID PROPELLANT MOTOR D. ATMOSPHERIC JET & THERMAL JET

D. ATMOSPHERIC JET & THERMAL JET

WHAT MISSILE CAN BE FIRED FROM THE TUBE LAUNCHERS INSTALLED ON VEHICLES, HELICOPTERS, OR FROM A TRIPOD ON THE GROUND? A. AGM-65 B. AGM-114 C. AIM-120 D. BGM-71

D. BGM-71

WHAT MISSILE IS A PRECISION WIRE GUIDED, HIGH VELOCITY, SHORT RANGE ANTITANK/ANTIARMOR, & BUNKER WEAPON? A. AGM-65 B. AGM-114 C. AGM-154 D. BGM-71

D. BGM-71

WHAT ARE THE TWO TYPES OF GENERAL FUZES USED IN GUIDED MISSILES? A. IMPACT & MECHANICAL B. IMPACT & ELECTRICAL C. CONTACT & ELECTRICAL D. CONTACT & PROXIMITY

D. CONTACT & PROXIMITY

THE CONTROL FINS SHOULD BE ATTACHED TO WHAT SECTION OF A SIDEWINDER GUIDED MISSILE? A. WARHEAD B. ROCKET MOTOR C. TARGET DETECTOR D. GUIDANCE & CONTROL

D. GUIDANCE & CONTROL

WHAT REUSABLE MISSILE LAUNCHER COMPLETES THE F/A-18 & P-3 AIRCRAFT SUSPENSION & LAUNCHING SYSTEM FOR THE AGM-65 MAVERICK MISSILE? A. LAU-7 B. LAU-115 C. LAU-116 D. LAU-117

D. LAU-117

ALL VERSIONS OF HELLFIRE MISSILES IN THE NAVY & MARINE CORPS INVENTORY ARE CARRIED ON WHAT TYPE OF GUIDED MISSILE LAUNCHER? A. ADU-299 & LAU-114 B. LAU-117 & LAU-118 C. LAU-118 & LAU-127 D. M-272 & M-299

D. M-272 & M-299

A MISSILE WITH A RATED SPEED OF MACH 3.2 IS FIRED FROM AN AIRCRAFT THAT IS FLYING AT A SPEED OF MACH 2.6. WHAT IS THE MISSILES ACTUAL SPEED AFTER BEING LAUNCHED? A. MACH 0.6 B. MACH 2.6 C. MACH 3.2 D. MACH 5.8

D. MACH 5.8

PASSIVE HOMING IS SIMILAR TO ACTIVE HOMING IN WHICH OF THE FOLLOWING WAYS? A. PASSIVE HOMING DOES NOT REQUIRE A CONTROL SECTION B. PASSIVE HOMING REQUIRES AN EXTERNAL SOURCE FOR A TARGET C. PASSIVE HOMING DOES NOT OPERATE INDEPENDENTLY OF THE LAUNCHING AIRCRAFT D. PASSIVE HOMING OPERATES INDEPENDENTLY OF THE LAUNCHING AIRCRAFT

D. PASSIVE HOMING OPERATES INDEPENDENTLY OF THE LAUNCHING AIRCRAFT

IN AN AIM-7M GUIDED MISSILE, THE WARHEAD IS BETWEEN WHAT TWO ASSEMBLIES? A. FLIGHT CONTROL SECTION & AUTOPILOT B. HYDRAULIC GROUP & AUTOPILOT C. TARGET SEEKER & AUTOPILOT D. TARGET SEEKER & FLIGHT CONTROL SECTION

D. TARGET SEEKER & FLIGHT CONTROL SECTION

SPEEDS FROM MACH 0.8 TO MACH 1.2 ARE REFERRED TO BY WHAT TERM? A. HYPERSONIC B. SUBSONIC C. SUPERSONIC D. TRANSONIC

D. TRANSONIC