SM Weapon's Test Flashcards

1
Q

What does the PDU do?

A
  • Consists of a circuit breaker box and a junction box
  • Circuit breaker box provides current overload and short circuit protection within the B
  • Junction box conditions power going to the CLT.
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2
Q

What is GDOP and what effects does it have?

A
  • The Geometric Dilution of precision. Indicates how much the geometric relationship of the tracked satellites affects uncertainty of the GPS receivers position.
  • Low values correspond to good geometry and are preferred.
  • It will not inhibit a launch
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3
Q

Where does the GPS feed come from?

A
  • TA-24
  • CMIGITs/SDN-500
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4
Q

What do you do if SAASM keys are not tracking?

A
  • Clear the keys and reload.
  • Recycle power to track the P(Y) code.
  • Clear them and recycle power.
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5
Q

When can you not enter INDOC mode?

A
  • With actual munitions (CLT connected)
  • Test fixtures (CATM, TIVA) should not be used in INDOC
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6
Q

Why do you enter INDOC mode?

A
  • Permits missions with simulated munitions inventory.
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7
Q

What is the BLK I footprint based off of?

A
  • Yellow line represents 80% of the max kinematic range (range based)
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8
Q

What is the BLK II footprint based off of?

A
  • B references DLL using 6DOF values for CEP90 (performance based)
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9
Q

When does the TSE disregard target reports from the seeker?

A
  • Less than 6 valid target reports or HIA and slant range to the target is greater than 2000 meters.
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10
Q

What are the conditions for the ESAF?

A

1) Canister ejection (starts 13.4 sec (+/-11%) digital timer
2) Umbilical disconnect
3) Wing deployment
4) Rocket Motor burn

Timers provide ~15 sec delay from ejection to warhead arming.

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11
Q

How does HIA work?

A
  • Missile can hold up to 12 degree AOA until reaching a calculated LOS angle to the grid location.
  • Missile flies directly to the grid when the MC/PCU computes approximately 70 degree impact angle is achieved
  • TSE does not accept seeker inputs until within 2000 m slant range passed
  • End game velocity = 600 ft/s
  • The missile favors velocity and will trade impact angle for velocity.
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12
Q

What BLK can be ground designated and why?

A
  • BLK III, it implements last pulse logic (LPL)
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13
Q

Why do you want a low PRF?

A
  • Lower codes are better for moving targets due to high PRF (sends more updates/higher refresh rate)
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14
Q
  • What is the TSE and what does it do?
A
  • Target State Estimator.
  • The missile always flies to the TSE-computed target location
  • After comparing target location and missile location, the TSE computes fin steering commands
  • The Griffin is not solely laser guided, but is TSE guided and laser assisted
  • Seeker azimuth and elevation translated into north, east and down directions and target velocity.
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15
Q

What are the improvements between blocks?

A
  • 1 - 2: Reliability
  • 2 - 3: Lethality
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16
Q

What are the parts of the Guidance Electronic Unit Assembly?

A
  • MC/PCU
  • I/O CCA
  • MEMS IMU
  • GPS receiver
  • GPS antenna
17
Q

What are the AGM-176 Sections?

A
  • Nose assembly
  • Warhead
  • Guidance Section
  • Wing Section
  • Adapter Section
  • Rocket Motor
  • Control Actuator Section
18
Q

What are the hazard class for the BLK II/III?

A
  • Total explosive hazard class: 1.2.1E
  • Warhead hazard class: 1.1D
19
Q

What are the low bias assumptions?

A
  • TSE assumes a flat Earth throughout the time of flight
  • To mitigate errors, a 50-meter low (HAE) bias is entered into the nav solution. Once the missile reaches within 25 m slant of the low bias, the missile zeroizes its fins and falls ballistic.
20
Q

What pieces of hardware does the B computer talk to?

A
  • TA-24
  • CMIGITs/SDN-500
  • B Control Box
21
Q

What are the 3 phases of the Paveway II trajectory?

A
  • Ballistic
  • Transition
  • Terminal
22
Q

What are the release envelope functions for the Paveway II?

A
  • Delivery airspeed
  • Dive angle
  • Altitude
23
Q

What is g-bias for the AGM-65L?

A
  • After launch a bias voltage is added to the vertical channel of the autopilot.
  • Missile lofts into a “humped” profile
  • Offsets gravity
  • Extends the aerodynamic range
  • Increases impact angle and velocity
  • Helps maintain LOS to the target