DS - Hellfire II Flashcards
(59 cards)
1
Q
The Hellfire missile is made up of four
main sections what are they?
xx
A
- Guidance Section
- Warhead Section
- Propulsion Section
- Control Section
2
Q
Guidance Section consists of what 2 groups?
A
Sensor Group
Guidance Electronic Group
3
Q
Guidance Section contains components to conduct what?
5
A
Search Detect Acquire Process Track laser energy
4
Q
What targets is the Hellfire missile
designed to attack? (6)
A
- Ships superstructures
- Deck mounted weapon systems
- Light Armoured Vehicles
- Trucks
- Light bunkers
- Buildings
5
Q
The strakes on the Guidance section are
designed for what?
A
Provide stability during flight
6
Q
What is the ESAF arming sequence?
5
A
- Power on
- Built in Test (BIT) has passed
- Umbilical separation
- Fuze data
- Safety separation have been received in the proper sequence
7
Q
The MC warhead assembly consists of:
7
(pic on slide 42)
A
Warhead case Liner, Explosive billet Wave shaper, Aft closure Precision Initiation Charge (PIC) Retainer ring
8
Q
Tab Data - Range: Min to Max Weight: NEQ: Speed: Time of flight: - to 3.75km ? - to 8km? HCC: 1.1E
A
Range: 500m to 8,000m
Weight: 49kg
NEQ: 12.447kg
Speed: Mach 1.3
Time of flight: 12s to 3.75km
37s to 8km
HCC: 1.1E
9
Q
Modes of Operation xx
Lock on Before Launch (LOBL) - Min- max range? Lock on after Launch (LOAL). Provide min/max ranges: - Direct - Low - High Each mode provides a different...what ?
A
Modes of Operation Lock on Before Launch (LOBL) - 500m - 7000m Lock on after Launch (LOAL) - Direct: 1500 - 7000m - Low: 2000 - 8000m - High: 3500 - 8000m Each mode provides a different FLIGHT TRAJECTORY SHAPE
10
Q
What gases power the Hellfire gyroscope?
A
Nitrogen and Freon
11
Q
Different types of rounds?
3,1,2
A
-Tactical
-Captive Air Training Module (CATM)
Dummy (DATM)
- Blue
- Grey
12
Q
Missile consists of what class of guidance system?
A
- Semi -automatic Laser guidance section
13
Q
Look at thermal battery pic. And give the following info:
- Activated by?
- Operating temp
- Battery time
- Volts
- Temp at which the battery output is terminated; what effect happens?
A
- EED
- 260 oC
- 55 sec
- 28 volts
- 204 oC
- solidification of the electrolyte takes place
14
Q
What are the incendiary elements
- their mass
- what are they designed for.
A
Zirconium Sponge pellets 218g
- Ignite and burn combustibles and ordnance
15
Q
Label Hellfire
A
…
16
Q
What does the control interface group (CIG) provide?
What does it consist of?
A
- Provides electrical power
- pneumatic power for fins
- control signals to actuate fins
Pneumatic Accumulator 8,800 psi
Thermal battery
Control Interface Assembly (CCA?)
17
Q
How does the AGM 114 ESAF work?
A
- Using digital circuitry to control the exploding foil initiator
- and slapper type detonator which is physically in line with the warhead charge
18
Q
Safe & Arm Device needs what voltage to work?
A
28 vDC
- Rotates the rocket motor squibs to an in-line position
19
Q
Safe & Arm Device
When will the SAD return to the SAFE position?
What is the maximum time the SAD should be energized?
A
- If SAD returns to zero volts
- one minute
20
Q
Hellfire warhead
- Main Charge (MC)
- Fill and weight?
- booster?
A
PBXN-9
- 2815 g
PBXN-5
- 315mg
21
Q
Hellfire warhead
- Precursor Charge (PC)
- Fill and weight?
- booster?
A
PBXN-9
- 486 g
PBXN-5
- 200mg
22
Q
Hellfire Propellant?
A
GEU
9120 g
23
Q
HELLFIRE OPERATION SEQUENCE…..?
A
read it
24
Q
RBS 70
Missile-in Container (MiC) components? (6)
A
End Caps Launcher Tube Missile Lock Missile Launch Motor Bolide Missile
25
Name the RBS 70 sections?
-Rear Section
-Sustainer Motor
-Forward Section
(Warhead)
26
Name the components of the RBS 70 Warhead section?
Explosive charge
| Proximity Fuze
27
RBS 70 NEQ
HCC
5. 354 kg
| 1. 2E
28
RBS 70 Warhead
- Main charge fill and weight?
- What is the fragmenting fill and qty?
OCTOL (HMX/TNT)
- 475 g
3,000 Tungsten spheres
29
RBS 70 is what type of guidance system ?
- SACLOS
30
What is the maximum range of the RBS 70
- 8000m
| - height of 5000m
31
- How long does the RBS 70 launch motor burn?
- resulting velocity?
- Sustainer motor?
- 40 milliseconds
- 50m/s
5 seconds
32
The missile rear Section consists of what?
Electronic Package (EP) No. 3
Control section
EP 2
Missile Battery
33
How many nozzles are there and why are they plugged?
- 4
| - to prevent ingress of moisture
34
What makes the Bolide man portable?
What 3 parts?
MIC ready to go in 30 seconds broken into 3 parts
- stand,
- sight
- Missile assembly
35
What protects the Bolide during storage and transport?
Protected against mechanical damage by - shock absorbing cellular plastic end caps
- and a centre pad
36
What features are included in the warhead of the Bolide?
Multiple effects warhead combining blast, frag, and shaped charge
37
What are the three modes of operation of the proximity fuze;
What is the minimum and maximum target detection ranges on the Bolide?
Off, Normal and Small Target
0.4 sec and 6 sec
38
RBS 70 Launch Motor
| - What does the fixed stud nozzle do to the motor jet and why?
- deflects the motor jet by 2 degrees
| - to compensate for gravity
39
How is the Bolide missile guided to the target?
By a laser beam generated on the sight, forming a guidance corridor
40
RS 70 Initiation devices?
A beam riding missile that provides extended range and features an
adaptable proximity and impact fuze
41
RBS 70 what is the role of the shackle unit?
To secure the missile to the launch motor in the container.
42
RBS 70 SAD....
...
43
RBS 70 OPERATION (22)
```
• Upon firing button pressed:
• The thermal battery initiated 0.2 --.05 sec
• Missile gyro initiated
• Missile electronics begin
• Nozzle spoiler activation
• Release of missile lock
• Ignition of launch motor
• Leads ripped off missile (EP1 interface)
• After 5mm movement shackle unit released
• Recoil motors ignite (reducing recoil)
• Missile leaves launch tube
• Wings unfold and lock into position
• Two wing switches close circuit
• Ignition impulse to ignite Sustainer motor
• Sustainer motor fires
• 7 G’s acceleration closes SAD circuit
• SAD stepper motor aligns firing train
• EP3 detector tracks transmitter beam
• EP1 analyses transmitter strength and provides course corrections to the rudders through the rudder mechanism
• Missile closes with target
• Detection and functioning
• as per PROX mode Functioning
- Off, Normal, Small Target
```
44
RBS 70
| What is the Proximity Fuze Transmitter got?
- 18 x narrow lobes
| - directed forward at 30 degree angle
45
What four components make up the Javelin Missile?
- Guidance section
- Main warhead section (Midbody section)
- Propulsion section
- Control section
46
What are the six phases of operation for the Javelin?
```
CLU preparation, cool down and standby
Activate AUR
Target Track
Launch
Flight Control
Warhead detonation
```
47
How long does the firer hold the trigger on the Javelin when launching?
- Minimum of 400 milliseconds
48
What distance is safe separation declared on the Javelin?
What time of flight?
- 41.5 meters
| - bxn 0.75 and 1.8 sec
49
What pressure does the Javelin BCU:
- Operating pressure
- vent pressure?
- 7,500 psi
| - Vent at 13,900 psi
50
What signals are required by the ESAF/CESAF prior to firing the warheads of the Javelin?
- Missile fin lock
- Missile safe separation
- Missile ‘good guidance’ from GEU
51
CESAF is made up of two parts:
```
Electronics Module (EM)
Firing Modules (FM)
```
52
S&A Mech, Components
-
53
Make up of the Precursor warhead
Diameter
Fill type
weight
- 60mm
- LX-14
- 372 g
54
Make up of the Precursor and Main warheads
- Liner type
- fill type
- fill weight
- Main
- Molybdenum shaped charge liner
- LX-14
- 1422 g
55
Tab data of the Battery Coolant Unit (BCU)
Battery life?
- Activation?
- What colour is the status indicator when used?
- Prior to use?
- 4 minutes
- Activation by electro-explosive device as part of the firing sequence
- Black
- Clear
56
Launch events sequence
- Gunner attaches CLU to the LTA
- Forward end cap removed
- Target acquired, either with optics or the Thermal Imaging (TI) sight
- Gunner activates missile seeker by pulling left trigger on CLU
- After approximately 9.5 secs the missile seeker cools down
- Flight software data is downloaded and missile becomes operational
- Once missile is operational infrared imagery from seeker is viewed by gunner through CLU
- Tracker software data downloaded from CLU to missile
- Gunner then positions track gates to specify the target portion of the seeker image
- Target maybe engaged either by DA or OTA
- On completion of target lock on gunner depresses CLU fire trigger
- Depression of trigger fires missile restraint pin squib to fire
- On successful completion of pre launch tests software issues command to fire launch motor
- Overpressure from LM opens aft membrane and propels missile forward
- Forward motion fractures forward seal and severs umbilical cable and gas line interfaces Missile continues along LTA until missile wings and fins clear the LTA
- Once clear of LTA and confirmation of correct launch, missile software issues command to ignite FM
- Warhead is armed following safe separation distance from operator determined by CESAF module
- Seeker and tracker software continues to track target to impact without intervention by gunner
57
What does the Javelin system consist of?
- Command Launch Unit (CLU)
| - All Up Round (AUR)
58
What are the four methods of operation of the CLU?
Off
Day
Night
Test
59
```
What type and thickness of armour is the
Javelin missile designed to defeat?
-Frontal armour
-Side armour
-Top armour
```
- ERA with 100mm RHA
- ERA and 80mm RHA
- ERA and 50mm RHA
