DS - Hellfire II Flashcards

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
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2
Q

Guidance Section consists of what 2 groups?

A

Sensor Group

Guidance Electronic Group

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3
Q

Guidance Section contains components to conduct what?

5

A
Search
Detect
Acquire
Process
Track laser energy
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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
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5
Q

The strakes on the Guidance section are

designed for what?

A

Provide stability during flight

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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
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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
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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
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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
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10
Q

What gases power the Hellfire gyroscope?

A

Nitrogen and Freon

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11
Q

Different types of rounds?

3,1,2

A

-Tactical
-Captive Air Training Module (CATM)
Dummy (DATM)
- Blue
- Grey

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12
Q

Missile consists of what class of guidance system?

A
  • Semi -automatic Laser guidance section
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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
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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

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15
Q

Label Hellfire

A

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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?)

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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
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18
Q

Safe & Arm Device needs what voltage to work?

A

28 vDC

- Rotates the rocket motor squibs to an in-line position

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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

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20
Q

Hellfire warhead

  • Main Charge (MC)
  • Fill and weight?
  • booster?
A

PBXN-9
- 2815 g

PBXN-5
- 315mg

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21
Q

Hellfire warhead

  • Precursor Charge (PC)
  • Fill and weight?
  • booster?
A

PBXN-9
- 486 g

PBXN-5
- 200mg

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22
Q

Hellfire Propellant?

A

GEU

9120 g

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23
Q

HELLFIRE OPERATION SEQUENCE…..?

A

read it

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24
Q

RBS 70

Missile-in Container (MiC) components? (6)

A
End Caps
Launcher Tube
Missile Lock
Missile Launch Motor
Bolide Missile
25
Q

Name the RBS 70 sections?

A

-Rear Section
-Sustainer Motor
-Forward Section
(Warhead)

26
Q

Name the components of the RBS 70 Warhead section?

A

Explosive charge

Proximity Fuze

27
Q

RBS 70 NEQ

HCC

A
  1. 354 kg

1. 2E

28
Q

RBS 70 Warhead

  • Main charge fill and weight?
  • What is the fragmenting fill and qty?
A

OCTOL (HMX/TNT)
- 475 g

3,000 Tungsten spheres

29
Q

RBS 70 is what type of guidance system ?

A
  • SACLOS
30
Q

What is the maximum range of the RBS 70

A
  • 8000m

- height of 5000m

31
Q
  • How long does the RBS 70 launch motor burn?
  • resulting velocity?
  • Sustainer motor?
A
  • 40 milliseconds
  • 50m/s

5 seconds

32
Q

The missile rear Section consists of what?

A

Electronic Package (EP) No. 3
Control section
EP 2
Missile Battery

33
Q

How many nozzles are there and why are they plugged?

A
  • 4

- to prevent ingress of moisture

34
Q

What makes the Bolide man portable?

What 3 parts?

A

MIC ready to go in 30 seconds broken into 3 parts

  • stand,
  • sight
  • Missile assembly
35
Q

What protects the Bolide during storage and transport?

A

Protected against mechanical damage by - shock absorbing cellular plastic end caps
- and a centre pad

36
Q

What features are included in the warhead of the Bolide?

A

Multiple effects warhead combining blast, frag, and shaped charge

37
Q

What are the three modes of operation of the proximity fuze;

What is the minimum and maximum target detection ranges on the Bolide?

A

Off, Normal and Small Target

0.4 sec and 6 sec

38
Q

RBS 70 Launch Motor

- What does the fixed stud nozzle do to the motor jet and why?

A
  • deflects the motor jet by 2 degrees

- to compensate for gravity

39
Q

How is the Bolide missile guided to the target?

A

By a laser beam generated on the sight, forming a guidance corridor

40
Q

RS 70 Initiation devices?

A

A beam riding missile that provides extended range and features an
adaptable proximity and impact fuze

41
Q

RBS 70 what is the role of the shackle unit?

A

To secure the missile to the launch motor in the container.

42
Q

RBS 70 SAD….

A

43
Q

RBS 70 OPERATION (22)

A
• 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
Q

RBS 70

What is the Proximity Fuze Transmitter got?

A
  • 18 x narrow lobes

- directed forward at 30 degree angle

45
Q

What four components make up the Javelin Missile?

A
  • Guidance section
  • Main warhead section (Midbody section)
  • Propulsion section
  • Control section
46
Q

What are the six phases of operation for the Javelin?

A
CLU preparation, cool down and standby
Activate AUR
Target Track
Launch
Flight Control
Warhead detonation
47
Q

How long does the firer hold the trigger on the Javelin when launching?

A
  • Minimum of 400 milliseconds
48
Q

What distance is safe separation declared on the Javelin?

What time of flight?

A
  • 41.5 meters

- bxn 0.75 and 1.8 sec

49
Q

What pressure does the Javelin BCU:

  • Operating pressure
  • vent pressure?
A
  • 7,500 psi

- Vent at 13,900 psi

50
Q

What signals are required by the ESAF/CESAF prior to firing the warheads of the Javelin?

A
  • Missile fin lock
  • Missile safe separation
  • Missile ‘good guidance’ from GEU
51
Q

CESAF is made up of two parts:

A
Electronics Module (EM)

Firing Modules (FM)
52
Q

S&A Mech, Components

A

-

53
Q

Make up of the Precursor warhead

Diameter
Fill type
weight

A
  • 60mm
  • LX-14
  • 372 g
54
Q

Make up of the Precursor and Main warheads

  • Liner type
  • fill type
  • fill weight
A
  • Main
  • Molybdenum shaped charge liner
  • LX-14
  • 1422 g
55
Q

Tab data of the Battery Coolant Unit (BCU)

Battery life?

  • Activation?
  • What colour is the status indicator when used?
  • Prior to use?
A
  • 4 minutes
  • Activation by electro-explosive device as part of the firing sequence
  • Black
  • Clear
56
Q

Launch events sequence

A
  • 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
Q

What does the Javelin system consist of?

A
  • Command Launch Unit (CLU)

- All Up Round (AUR)

58
Q

What are the four methods of operation of the CLU?

A

Off
Day
Night
Test

59
Q
What type and thickness of armour is the
Javelin missile designed to defeat?

-Frontal armour
-Side armour
-Top armour
A
  • ERA with 100mm RHA
  • ERA and 80mm RHA
  • ERA and 50mm RHA