LO Principles Flashcards

1
Q

Objective of stealth

A

Increase survivability by REDUCING THE PROBABILITY OF DETECTION and exposure to engagement by threat system

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2
Q

Describe active signature/ examples

A

ALL THE OBSERVABLE EMISSIONS FROM AN AIRCRAFT

  • RF Signals: comm, navigation, radar
  • Acoustic: engine noise, prop noise
  • Infrared: engine exhaust, skin temp
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3
Q

Describe passive signature/examples

A

ALL THE OBSERVABLE SIGNALS FROM AN AIRCRAFT RESULTING FROM EXTERNAL ILLUMINATION

  • EO/Visual
  • EM (radar)
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4
Q

Countering RF Active Signature Collectors:

Counter threat data collectors with ____________ designs.

A

Low Probability of Intercept (LPI)

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5
Q

Acoustic Signature Reduction: _________ are the primary source of noise

A

Engines

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6
Q

Radar signature is dominated by………

A

Shape

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7
Q

Why is RCS the most critical signature of most aircraft?

A

Radar provides all weather, long range detection capability (early warning)

Radar provide target range, azimuth, and velocity data (target tracking)

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8
Q

Stealth is enhanced by …. (3)

A
  • Forcing Threats to use active sensors sparingly
  • Using intel data to minimize onboard active and passive sensor exposure
  • Use tactics that combine w/ order of battle as well as man made environment
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9
Q

Define RCS

A

RADAR SIGNATURE IS EXPRESSED AS AIRCRAFT RCS.

  • Amount of energy scattered back to radar by a target
  • Measure of power expressed as dBsm
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10
Q

Explain the factors that determine RCS size

A

Target Aircraft Factors: Azimuth, Elevation

Viewing Radar Factors: Frequency, Polarization

*** Vertically polarized waves generate significant return from wing TRAILING EDGES; Horizontally –> wing LEADING EDGES.

*** To reduce detection range by half (3 dB), the RCS must be reduced by 16

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11
Q

List 4 basic methods to make an aircraft stealthy

A

SHAPING (most important)

Absorption

Cancellation

Transparencies

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12
Q

Describe shaping

A

Reflect radar energy into any direction other than back to the radar site.

***AIRCRAFT SHAPING TO BOUNCE ENERGY IN SPIKES***

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13
Q

Describe absorption

A

Utilize RAM to turn radar energy into heat

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14
Q

Describe cancellation

A

Actively or passively reflected radar waves add together to cancel each other out

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15
Q

Describe transparencies

A

Allow radar energy to pass thru the material w/ minimal reduction in energy or change in wave characteristics

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16
Q

Describe faceted shaping

A

Orient flat surfaces to deflect radar energy away from threat radar

example: F117

17
Q

Describe compound curve

A

Replace straight edges with curved edges to reflect less radar energy towards threat radar

Example: B2

18
Q

Describe planform alignment

A

Return a radar signal in a very specific direction away from the radar emitter (all in the same alignment)

Example: F22

19
Q

Goals of radar absorption materials

A
  • Reduce specular and multibounce reflections
  • Reduce energy diffracted from trailing edges or discontinuities by absorbing energy as the wave travels along the surface
20
Q

List types of absorbers

A
  • Resonent absorber (specific frequency)
  • Nonresonant absorber (range of frequencies)
21
Q

Characteristics of E-RAM

A

Resonant, causes waves to cancel each other out

  • Narrowband
  • Thick, but light
22
Q

Characteristics of MagRAM

A

Nonresonant, coating with ferromagnetic materials

  • Broadband
  • Thin, but heavy
23
Q

Characteristics of large volume RAS

A

Nonresonant, radar absorbant structure

  • Broadband
  • Thick, but light
24
Q

How does the aircraft surface breaks and gaps affect total RCS

A

Residual reflections are caused by surface discontinuities, more significant with higher frequencies.

Reflections reduced by:

  • Coating aircraft with RAM
  • Filling gaps with RAM
25
Q

Engine inlet design methods used to reduce RCS

A
  • Screen grids
  • Buried engines
  • Intakes on top
26
Q

Canopy design methods used to reduce RCS

A
  • Made of radar absorbing materials with a metallic coating
  • Smoothly blended into aircraft
  • Shape deflects radar away
27
Q

Other considerations/methods used to reduce RCS

A
  • Antennas
  • Windows for sensors
  • Air data sensors
  • Access doors
  • External stores
28
Q

List 4 basic systems used to counter stealth

A
  • Low freq radar
  • High freq radar
  • Bi/multi static radar
  • Passive coherent radar
29
Q

2 limitations of low freq radar

A
  • Few frequencies available and heavy clutter
  • Poor range resolution
30
Q

2 limitations of high freq radar

A
  • Short range
  • Atmospheric attenuation
31
Q

2 limitations with bi/multistatic radar

A
  • Synchronization
  • Widebeam antenna or long scan time
32
Q

2 limitations of coherent radar

A
  • Reliance on third party illuminators
  • Azimuth/range only

“Listening to white noise… then aircraft comes along and disrupts the noise”

33
Q

Discuss mx practices that assure LO properties

A
  • Mx tracking records
  • Visual inspections
  • Mechanical Verification
  • Material reflective measurements
  • True RCS measurements
  • Diagnostic imaging
  • Special Facilities
34
Q

Discuss elements that contribute to cost of stealth

A
  • Cost per flying hr
  • Acquisition cost
  • Infrastructure cost (security, support, etc…)
  • Inspection cost
  • Personnel cost
35
Q

What is the value of stealth

A
  • provides a method of breaking the kill chain

GREATER SURVIVABILITY EQUALS REDUCED RISK OF KILL CHAIN BEING COMPLETED.

36
Q

Discuss limitations of stealth

A
  • Operating cost
  • Limited number of assets
  • Complex MSN Planning
  • Lacks flexibility
  • Threats