DS - RBS 70 Flashcards

1
Q

RBS 70 - Missile Components (6)

A
MiC - Missile in Container
End caps
Launcher tube
Missile lock
Missile launch motor
Bollide missile
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2
Q

.

A

..

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3
Q

Rear End Cap Safety Device…..

A

.

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4
Q

.

A

.

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5
Q

.

A

.

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6
Q

.

A

.

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7
Q

.

A

.

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8
Q

Launch motor Propellant, 3 parts:

Igniter
Igniter Charge
Grain

A

  • 460g NK1256 DB
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9
Q

3 main components of the RBS 70

A

Stand
Sight
MiC (missile in container)

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10
Q

What is the role of the end caps

A

Provide protection for the launch tube

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11
Q

Speed of the missile in the tube?

A

50 m/sec

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12
Q

What guidance and initiating devices does Bolide have?

A

Beam riding missile with extended range to older variants and has adaptable proximity and impact fuze

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13
Q

What is the NEQ of Bolide?

A

5.34kg

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14
Q

What does MiC stand for?

A

Missile in Container

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15
Q

What is the NEQ of Bolide? Including Propellant

A

5.34kg

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16
Q

What is the launch motor burn time of the Bolide?

A

Approximately 40m/s

17
Q

In the Bolide, what components does the EP2 contain and what function do they perform?

A

LP2 contains the thermal battery, voltage converters and stabilisers used to produce the missile electrical power

18
Q

What is the launch motor burn time of the Bolide?

A

Approximately 40m/s with burnout occurring within the launch tube

19
Q

Describe the shape and dispersive effects of the casing of the warhead on the Bolide?

A

The casing has a convex contour to provide an effective dispersion of fragments both forwards and rearwards

20
Q

What additional layers are used in the warhead and what is contained in that layer which enhances frag effect for the Bolide?

A

A plastic layer around the steel casing containing approximately 3000 tungsten spheres to enhance frag

21
Q

Warhead Section

  • Explosive Charge type
  • Charge weight
  • Material and number of spheres
  • Shaped charge?
A
  • Octol (HMX/TNT)
  • 0.475kg
  • 3,000 tungsten spheres
  • Yes (but not by design)
22
Q

Prox Fuze

  • Minimum detection
  • Maximum detection
A
  • 0.4m
  • 6m
  • 4m
23
Q

Prox Fuze
Transmitter - describe

xx

A

18 lobes

directed forward at 30 degrees

24
Q

Prox modes

A

Off
normal
small target

25
Q

Max flight time for Auto Destruct

A

40 sec

26
Q

RBS70 Operation

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