1
Q
4 Major Sections
A
- Guidance
- Warhead
- Propulsion
- Control
2
Q
Gases contained in the displacement gyroscope
A
Nitrogen and Freon
3
Q
What is the incendiary capability?
A
218g of Zirconium Sponge Pellets
4
Q
Label Diagram - Guidance Section
A
- Seeker
- Guidance Electronics Group
- Gyroscope
- Shotgun connector
5
Q
Label Diagram - Warhead Section
A
- Zirconium Sponge
- PBXN-109 Main Charge
- Blast Fragmentation Warhead
- PBXN-5 Booster
- BF-ESAF with TD Fuze Assembly
- Pneumatic Accumulator
- Thermal Battery
6
Q
Label Diagram - Propulsion Section
A
- Control Interface Assembly
- Rocket Motor
- Spider Spacer
7
Q
The Control Interface Group (CIG) provides what?
A
- 28 vdc missile power
- 600 psi nitrogen/freon for flight control actuators
- interfaces for squib activations
- Control signals to fin actuators
8
Q
What are the Thermal Battery temperatures?
A
After initiation - 260 degrees C
Output - 28 volts for min 55 secs
Output termination - 204 degrees C
9
Q
What type of initiator/Detonator does it use?
A
Exploding Foil initiator (EFI), slapped type detonator
Ammunition Technician
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