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Just The Two Of Us > ASE > Flashcards

ASE Flashcards

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1
Q

Where is the AN/APR–39 radar warning receiver(RWR) digital processors located in the aircraft?

A

Left avionics bay

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2
Q

Which component provides radar, laser, and missile threat audio to the crewmembers?

A

Communication interface unit (CIU)

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3
Q

Where are RWR,LWR and MWS detected threats displayed on the ASE and TSD pages of the multipurpose display?

A

ASE threat symbols are always displayed on the inside of the ASE footprint

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4
Q

When will an ASE footprint be displayed on the TSD page?

A

When ASE threats are selected for presentation from the TSD-Threat/SHOW page and at least one threat exist for display

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5
Q

How may the AN/APR39A radar warning receiver (RWR) be declassified?

A

Remove the User Data Module (UDM)

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6
Q

What is the purpose of the blade antenna within the RWR system?

A

Receives C/D band radio, frequency, energy, and routes it to the digital processor

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7
Q

What indication does the AN/APR–39 RWR PROVIDE IF THE RECEIVED THREAT DETECTION DOES NOT MATCH A STORE THREAT IN THE EID file?

A

A “U” Will be displayed

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8
Q

How can the crew identify the systems number one priority ASE emitter when looking at the ASE or TSD pages?

A

The emitter will have a Homeplate symbol surrounding it

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9
Q

Which component contains a classified operational software required for tactical operation of the laser detecting set (LDS/LWR)?

A

The user data module (UDM)

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10
Q

What three threats are detected by the LDS/LWR?

A

Beam rider, designator, and range finder

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11
Q

How many degrees of detection are provided by the LDS/LWR in elevation?

A

+-45

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12
Q

How many degrees of detection are provided by the LDS/LWR in azimuth?

A

360

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13
Q

The AN/AVR–2B laser detector set is designed to operate in conjunction with which other ASE system?

A

APR-39 RSDS/RWR

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14
Q

The RFI gives the crew 360° of coverage. What numeric values define the fine area?

A

90°, with 45° each side of the FCR centerline

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15
Q

What is the primary difference between the fine and coarse areas of coverage?

A

Azimuth accuracy is much better than the fine area of coverage.

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16
Q

What three types of radar systems can RFI detect?

A

Pulse, Pulse Doppler, and Continuous Wave

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17
Q

What is a primary function of the RFI system?

A

It functions primarily as an offensive system that provides an FOV target cueing for onboard and offboard sites/sensors for employment of weapons.

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18
Q

What identifies an emitter that has been detected in the fine area of coverage of the RFI antenna array?

A

A triangle at the bottom center of the symbol

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19
Q

On what three FCR operational modes will RFI icons be displayed?

A

GTM, RMAP, ATM

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20
Q

How can you differentiate between a priority emitter that is tracking/missile guidance from another platform and an emitter that is signal, lost, lock, broken, or undetermined?

A

Home plate intensity

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21
Q

How many RFI emitters can be displayed on the FCR, ASE and TSE pages?

A

10

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22
Q

What symbology indicates an MRFI interim solution?

A

A line with increasing/decreasing Chevrons

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23
Q

What two configurations can MRFI be installed?

A

FCR (pinned) and URX

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24
Q

What is the advantage of MRFI over RFI?

A

Passive location of threats

25
Q

How many ASE emitters (RWR,LDS, MWS) can be displayed on the FCR page?

A

None

26
Q

RFI detected/Emitter symbols will not be selected via the CAQ function on either the ASE or TSD pages when the___ is the selected site

A

FCR

27
Q

What two pages are used to enable the RFI system if it is installed on the aircraft?

A

FCR UTIL or weapon UTIL (Cpg or plt)

28
Q

How can the Kruse select a non-priority radar frequency interferometer threat to conduct a cued search on?

A

Reselect the cued search button and/or use the cursor select function to choose an emitter

29
Q

What four functions are performed when the cued search button is selected?

A

1.FCR centerline slews in azimuth to RFI #1 emitter
2. FCR is placed in the proper mode , unless already there.
3. Set the appropriate scan size, as determined by how the threat was detected.
4. Scan will be automatically initiated.

30
Q

How is a manual Cued search performed?

A
  1. An emitter is selected from the FCR page.
  2. A single scan is initiated.
31
Q

What indication does a crew receive if an emitter has been merged?

A

The RFI icon will appear within the FCR footprint as the NTS

32
Q

When performing an automatic cued search utilizing the LHG, what will the FCR mode to if it is an airborne type emitter and the FCR is in the TPM mode?

A

ATM mode with a narrow field of view scan

33
Q

In order for the crew to perform a manual cued search when the FCR is the LOS, the RFI threat emitter must be selected from the___ page utilizing the cursor select method

A

FCR

34
Q

What is the function of the CWS system?

A

Used to detect and in conjunction with the ICMD, counteract IR missile threats

35
Q

What component serves as a primary processing center for LWR, RWR, and CMWS systems?

A

Aircraft gateway processor (AGP)

36
Q

What component houses the user data module for CMWS?

A

ECU

37
Q

How can the AN/AAR–57 (V) be safed in addition to selecting the safe/arm button on the ASE, WPN, or Init page?

A

By installing the safety pin in the safety switch

38
Q

Where are the HFI detect displayed on the ASE page?

A

Inner ring of the ASE footprint

39
Q

Sites and weapons can immediately be cued to the azimuth of the HFI threat. True/false.

A

True

40
Q

What are the 2 CMWS declared hostile fire threats?

A

Gunfire and RPG

41
Q

The ASE auto store only applies to which type ASE points?

A

MWS Geo located points and MRFI points

42
Q

Which page are ASE Geo located stored points displayed on?

A

TSD

43
Q

In order to auto transmit a Geo located ASE point the CMDS system must be____

A

Armed

44
Q

How many ASE Geo located points can be stored in the COORD file?

A

60, but can be indexed to 99

45
Q

What do bearing lines indicate?

A

Pairs of Geo located ASE threat with a detecting platform at the time of detection. Altitude of detecting platform is displayed in MSL.

46
Q

During an automatic dispense of flares is the air crew required to provide inputs to CMWS?

A

No

47
Q

What 3 CMDS status indications are displayed in the CM inhibit status windows?

A

Arm, safe, or PIN

48
Q

What 3 CMDS status indications are displayed in the HMD HAD?

A

Current manual program, safe or PIN

49
Q

When arming the CDS system utilizing the stores jettison panel, who can perform the jettison function?

A

Plt or CPG

50
Q

Where are the manual dispense controls located for the CMWS?

A

Cyclic stick

51
Q

What capabilities are lost in an “ASE BACKUP” condition?

A

No ASE threat displays or audio. No inventory/fault status.

52
Q

What conditions will cause the jettison feature to be inhibited?

A

Engaging either of the two system safeties, CMDS safety pin or weight on wheel switch (squat)

53
Q

What capabilities are lost in a “CMDS BYPASS” condition?

A

No automatic dispense. Limited manual dispense. No inventory/fault status. No display/audio if MWS fails.

54
Q

CIRCM may lase missile regardless if CMWS declares the threat. True/false.

A

True

55
Q

How does the crewmember arm the laser for the CIRCM system?

A

Selecting R JAM button on ASE page

56
Q

What indication will you see when CIRCM is lasing a threat?

A

Lightning bolt in center of own ship

57
Q

How can M206 and M211 munitions be identified?

A

The M206 has a red endcap with a letter “F” on it.
The M211 has a gray sealant on the end

58
Q

How is the MIDAS payload module installed in the dispenser?

A

Red down and out

Just The Two Of Us (2 decks)

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