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62 Cards in this Set
- Front
- Back
What level of thrust is required in order for the missile to separate from the launcher and what must be overcome in the AGM 114 series? |
2670N to overcome the hold back latch |
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What are the safety arrangements within the electro sub assembly in the AGM 114 series? |
Detonator held out of line Leads shunted and earthed |
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What is the weight and fill of the Propulsion section in the AGM 114 series? |
7.21kg of MIS 35903 1.86kg of MIS 35903 |
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What does the CIG provide electrical power for in the AGM 114 series? |
Control Section ESAF All EEDs Thermal battery Nitrogen pneumatic accumulator Pitch/roll gyro Rocket motor BIT and correct missile function |
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How is the ESAF powered in the AGM 114 series? |
Thermal battery power from the CIG |
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What are the three arming switches in the ESAF in the AGM 114 series? |
Acceleration and power (28V ac) received Fuze data transmission Safe separation |
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How is the precursor warhead initiated in the AGM 114 series? |
Warhead firing module |
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What is the blast dome designed to protect in the AGM 114 series? |
Main warhead |
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What is the type and weight of the precursor warhead filling in the AGM 114 series? |
1kg of PBXN-9 |
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What determines the choice of mode of operation for the GM AGM 114L? |
Moving or stationary target Distance |
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What is the principle operational difference between the 114K and 114L missiles? |
114K (Hellfire) uses a semi active laser 114L (Longbow) uses a millimetric radar |
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What is the purpose of the CEG in the AGM 114 series? |
It guides and steers the missile onto the target |
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When would a missile enter decorrelation in the AGM 114 series? |
When losing track of the target in the terminal phase |
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What allows multiple simultaneous engagements in the AGM 114 series? |
Apache radar sends two targets to the missile, a primary and secondary, with a pulse time coded laser |
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What is the difference between LOBL and LOAL? |
Lock on before launch tracks the target from before the point of launching Lock on after launch tracks the target after the missile has been fired |
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How is the frangible glass dome on the EPC shattered in the AGM 114K? |
Pneumatic actuator |
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What is the sensor group assembly designed to perform in the AGM 114 series? |
Target detect and tracking |
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What is the purpose of the spin torquer CCA in the AGM 114 series? |
Sends mirror/gyro commands from controller CCA to the sensor group |
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What does the propulsion section provide for the ESAF in the AGM 114 series? |
Acceleration to arm |
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What are the main components of the warhead section in the AGM 114 series? |
Main and precursor warheads High pressure nitrogen pneumatic accumulator ESAF |
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What does the High pressure nitrogen pneumatic accumulator provide? |
A supply of regulated filtered nitrogen gas to the control section at 4MPa |
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What are the visual differences between the 114K and 114L? |
114K is shorter with a clear glass dome 114L is longer with a white dome |
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What does the pitch/roll displacement gyro supply in the AGM 114 series? |
Body altitude and roll rate data for the auto pilot |
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What is the precursor warhead designed to provide? |
Initiation of ERA Clearance of the guidance section |
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How many 70mm rockets can be fitted to the WAH64 Apache helicopter? |
76 (19 per pod) |
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What range can 70mm rockets travel to? |
6.5km |
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What is the rate of fire for the 30mm chain gun? |
625 rounds per minute |
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What is the effective range of the 30mm chain gun? |
3.5km |
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What is the propulsion section in the AGM 114 series comprised of? |
Nozzle Rod/grain assembly Safe arm igniter assembly Case/Grain assembly |
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What is the rotator in the SAD in the AGM 114 series called? |
Solanoid |
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What are the major components of the Hellfire guidance section? |
Environmental Protection Cover Sensor Group Guidance Electronic Group |
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What is the Hellfire Guidance Electronics Group made up of? |
Motherboard and mechanical structure Controller CCA Sample and hold CCA Power supply Spin Torquer CCA |
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What are the Hellfire launch modes? |
LOBL LOAL Direct LOAL High LOAL Low |
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What is the range of the hellfire in LOBL? |
500m-7000m |
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What are the ranges and modes of the Hellfire in LOAL? |
Direct 1700-8000m Low 2000-8000m High 3500-8000m |
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What are the four trajectory stages of the AGM 114 series? |
Initial turn Mid course Terminal phase Decorrelation |
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Describe initial turn in the AGM 114 series |
Used for LOAL Direct mode + 4° pitch Low and high mode +20° pitch Ends on target correlation or +1.12s |
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Describe mid course in the AGM 114 series |
Nulls missile climb Maintains altitude Maintains straight line of flight Pitch +1° to +6° Ends on target correlation |
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Describe terminal phase in the AGM 114 series |
Used for LOBL and LOAL missile flies direct to impact on target Ends if target correlation is lost Restarts if target correlation is regained |
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Describe decorrelation in the AGM 114 series |
Used when target correlation is lost Missile flies on last line of sight of target Changes to terminal phase on target reacquisition |
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What does the longbow guidance section provide? |
Target acquisition Target tracking Missile guidance Autopilot functions Impact sensing |
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What is the longbow guidance section comprised from? |
Sensor group Guidance electronics group |
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What does the longbow radome protect against? |
RF (it only allows Ka band) |
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What is the longbow sensor group comprised of? |
Radome Antenna Ka band transceiver Gimbal assembly |
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What is the longbow guidance electronics group comprised of? |
Inertial measurements unit Electronic components assemblies Power supply Backplane assembly |
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What are the ranges of the longbow choice of mode operations? |
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What is the main warhead type and weight in the AGM 114 series? |
5.7kg of PBXN-5 |
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How is the main warhead of the AGM 114 series initiated? |
By the ESAF device main module |
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What is the difference between the AGM 114K-1 and 1A? |
The 1A has a fragmentation sleeve |
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What are the components in the ESAF in the AGM 114 series? |
Warhead firing module Cabling Main module |
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Describe the thermal battery in the AGM 114 series |
Fused salt type lithium alloy battery Stainless steel container EED initiated Provides 28V dc at 9 - 25.4 amps for 55 seconds |
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What does the control interface group (CIG) provide? |
Electrical power supply after launch High pressure nitrogen supply Electrical signal interface |
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What is the High Pressure Nitrogen Pneumatic Accumulator comprised of? |
Toroidal High Pressure Gas Reservoir 55MPA EED initiator Particle filter Pressure gas regulator Output port 4MPa |
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What does the control interface circuit card assembly in the AGM 114 series do? |
Controls arming and firing of missile Acts as interface between guidance section and other missile sections Serves as electrical power supply to other parts of the missile after launch |
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What are the CIG Interface Functions in the AGM 114 series? |
Initiation of thermal battery Initiation of high pressure nitrogen pneumatic accumulator Initiation of pitch/roll gyro Initiation of the rocket motor Arming delay and firing signals for the ESAF Control section actuator commands and fin positions Commands and signals necessary for BIT and correct missile function |
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Describe the action of the main warhead upon impact in the AGM 114 series |
Firing signal from the control interface CCA and ESAF device initiates the WFM attached to the precursor warhead ESAF device then initiates main module on the main warhead after specified delay |
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What are the AGM 114 series safety features? |
Arming only after successful BIT, missile/launcher separation and fuze data received and safe separation signals received in correct sequence Once armed, the ESAF device will not revert to the safe condition unless input power is removed from the main module An out of sequence arm command event permanently inhibits the arming of the ESAF device during flight |
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Describe the action of the warhead before impact in the AGM 114 series |
Arming sequence begins as missile is launched 28V passed to missile from aircraft immediately prior to launch. Controller CCA initiates a BIT of the ESAF device After a successful BIT and when 15V of power is applied ESAF device checks for missile/launcher separation to occur ESAF device monitors the longitudinal acceleration to determine if the safe arm distance has been reached During missile/launcher separation and the attainment of the safe arm distance the ESAF device receives fuze data message from guidance section general purpose processor This message is used to determine the detonation delay time between the precursor and main warheads When the ESAF safe arm distance has been reached the arming process continues ESAF device waits for a firing signal from impact sensor When ESAF is armed the firing capacitors in the WFM and Main Module begin to charge This sequence is complete before the motor is all burnt |
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Label the illustration of the through bulkhead assembly in the AGM 114 series |
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Label the illustration of the through bulkhead assembly in the AGM 114 series |
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How long will the motor burn for in the AGM 114 series and what speed will the missile be accelerated to? |
3 seconds 425 metres per second |
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What is the actuator assembly in the AGM 114 series comprised of? |
Potentiometers Output shaft assemblies Arm assemblies Piston assemblies Control valve assemblies |