2W051B Vol. 3 URE Questions I. Y. A. A. Y. A. S
Electro-optical
Light energy
Inertial
Radar
Infrared (IR)
Television
Inertial guidance
Imaging infrared (IIR)
Electro-optical
Light energy
Inertial
Radar
Active
Passive
Semi-active
Semi-passive
Active
Passive
Semi-active
Semi-Passive
Control
Guidance
Armament
Propulsion
Provide ballast in flight
Stabalize the weapon in flight
Steer the weapon to the target
Provide aerodynamics in flight
Provide ballast in flight
Stabalize the weapon in flight
Steer the weapon to the target
Provide aerodynamics in flight
Electro-servo actuators
Proportional
Electronic circuits
Pressurized fluid
A predertmined amount of time elapses
The missile senses the target getting closer
The missile senses the target moving farther away
The missile comes into direct contact with the target
Gas grain
Granular
Liquid
Solid
Igniting their rocket motors (R/M)
Damaging the internal circuits
Damaging the missile
Arming the fuze
Rocket motor (R/M), R/M igniter, and nozzle
Rocket motor (R/M), propellant, and nozzle
Fuel and rocket motor (R/M) igniter
Rocket motor (R/M) and R/M igniter
MK82
MK83
MK84
BLU-109
Computer unit, and a warhead section
Computer, and control section
Igniter, and computer control section
Control section, and warhead
Forward adapter assembly
Folding wing assembly
Control section
Control fins
Sends signals to the computer group which determines the direction to the target
Connects the GCU to the warhead
"Looks" for the reflected laser light signal
Holds the GCU seeker
Provide aerodynamic lift and stability during flight
Create smooth and stable flight while in glide mode
Provide steering commands for the control surfaces
Steer the bomb and provides aerodynamic lift
Provide an aerodynamic interface between the bomb and wing assembly
Extend the bomb charging well conduit to the hardback assembly
Provide more distance between the bomb and bomb rack
Provide the aerodynamic lift and stability during flight
WP 070 00
WP 080 00
WP 090 00
WP 998 00
Computer test set, AN/GJM-50
Digital test set, AN/GYQ-79
Digital test set TTU-395
Digital test set TTU-373
High pressure pnuematics
Invisible laser radiation
Equipment weight
High voltage
BLU-109
MK82
MK84
M117
FMU-139A/B
FMU-124A/B
FMU-113/B
FMU-143/B
Target detecting device (TDD)
Guidance section adapter
Guidance section
Control unit
MXU-724/B, MXU-724B/B, MXU-787/B, and the MXU-787A/B
MXU-724/B, MXU-724A/B, MXU-787/B, and the MXU-787B/B
MXU-724/B, MXU-742A/B, MXU-778/B, and MXU-778B/B
MXU-742/B, MXU-742B/B, MXU-778/B, and the MXU-778A/B
Provide guidance and location information to the computer unit during flight
Send signals to the computer to control the wings during flight
Send signals to the computer to determine direction
Steer the weapon during flight
Active imaging infrared (IIR)
Imaging infrared (IIR) only
Passive infrared (IR)
Television
AN/GJM-55
AN/GJM-65
AN/GJM-64
TTU-373
TTU-373
AN/GJM-55
AN/GJM-64
AN/GJM-65
Global positioning system (GPS) antenna, two moveable control fins, and two fixed find
GPS antenna, three moveable control fins, and one fixed fin
Three moveable control fins, and one fixed fin
And control fins
Allows the JDAM to reach a target without requiring the aircraft to directly overfly that target
Provides increased aircraft and aircrew survivablity
Allows the JDAM true "fire and forget" weapon capability
Provides increased weapons range
Tail assemblies
Aerosurfaces
Wings
Fins
GBU-31
GBU-32
GBU-38
GBU-54
GBU-24
GBU-31
GBU-32
GBU-38
GBU-38(V)1
GBU-38(V)4
GBU-54(V)1
GBU-54(V)4
GBU-39A/B
GBU-39/B
GBU-39/A
GBU-39
GBU-39A/B
GBU-39/B
GBU-39/A
GBU-39
137 pounds of a multi phased blast explosive (MBX)
37 pounds of a multi phased blast explosive (MBX)
36 pounds of a multi phased blast explosive (MBX)
16 pounds of a multi phased blast explosive (MBX)
30 or 33 feet
14 or 28 feet
7 or 14 feet
5 or 7 feet
Two
Three
Four
Five
Targeting information passed from the aircraft to the weapon
Weapon initiated built-in-test (IBIT)
Weapon release on aircraft command
Weapon power up sequence
Returned munitions inspection (RMI)
Storage monitoring insoection (SMI)
Carriage IBIT
Weapons IBIT
AN/GJM-396
AN/GYQ-79
AN/GJM-64
AN/GJM-65
Digital computer system assembly
Control box unit
Test adapter unit
Accessory kit
AN/GYQ-79 digital computer test set
Digital computer system assembly
Test adapter unit
Controller unit
Increased lock on and tracking of the missile to the target
Wider view of the battlefield to the pilot
"fire-and-forget" capability
Greater acquisition range
Imaging infrared (IIR)
Television guidance
Electro-optical
Semi-active
B
D
G
H
An auxiliary battery generator
A standard vehicle battery
A standard wall outlet
Its own batteries
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