THE FUTURE OF LOW-SIGNATURE PLATFORMS...THE FUTURE OF LOW-SIGNATURE PLATFORMS Anders Höök,...

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NOT COMPANY RESTRICTED | NOT EXPORT CONTROLLED | NOT CLASSIFIED THE FUTURE OF LOW-SIGNATURE PLATFORMS Anders Höök, Christer Larsson, Jakob Bjerkemo 2016-10-11 This document and the information contained herein is the property of Saab AB and must not be used, disclosed or altered without Saab AB prior written consent. 1 Funded by NFFP/Vinnova/FMV/Swedish Armed Forces

Transcript of THE FUTURE OF LOW-SIGNATURE PLATFORMS...THE FUTURE OF LOW-SIGNATURE PLATFORMS Anders Höök,...

Page 1: THE FUTURE OF LOW-SIGNATURE PLATFORMS...THE FUTURE OF LOW-SIGNATURE PLATFORMS Anders Höök, Christer Larsson, Jakob Bjerkemo 2016-10-11 This document and the information contained

NOT COMPANY RESTRICTED | NOT EXPORT CONTROLLED | NOT CLASSIFIED

THE FUTURE OF LOW-SIGNATURE PLATFORMS

Anders Höök, Christer Larsson, Jakob Bjerkemo 2016-10-11

This document and the information contained herein is the property of Saab AB

and must not be used, disclosed or altered without Saab AB prior written consent.

1

Funded by NFFP/Vinnova/FMV/Swedish Armed Forces

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THREAT DEVELOPMENT

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THREAT DEVELOPMENT

• Older radar systems were very range-capable

‒ S-200

• Today´s systems do not reach significantly longer...

• ... but are still much better

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S-200 Bar Lock S-200 Square Pair

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THREAT DEVELOPMENT

• Improvements:

‒ system bandwidth

‒ target update rates

‒ no. of tracked / engaged targets

‒ waveform agility

‒ multifunctionality (surv., tracking, fire control)

‒ tracking capability

‒ jamming resistance

‒ flexible search patterns

‒ frequency agility

‒ sidel-lobe blanking

‒ adaptive side-lobe cancellation

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LO AIRCRAFT AGAINST LRSAM RADARS

• Reducing range

‒ From: 450 km @ 0 dBm2

‒ To: Range km @ RCS dBm2

• Not very meaningful to use low RCS against LRSAM

‒ especially considering the low frequencies

• Thus termed:

‒ AA - Anti-Access

‒ AD - Area Denial

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Low-cost LO regime - aircraft

20 40 60 80

-10

-20

-30

-40

-50

-60

RCS (dBm2)

Range (km)

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SRSAM TRENDS

• No. of missiles per firing unit increases

‒ Tunguska 4

‒ Tunguska 8

‒ Pantsir 12

‒ Morfei 36 (?)

• Conclusion:

‒ Dimensioning against saturation attacks

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SRSAM TRENDS

• Increased update rate

• Turret aiming => vertical launch

‒ Tor, Morfei, MICA, IRIS T...

• Observation: response-time reduction

• Conclusion: dimensioning against:

‒ high-velocity missiles

‒ @ low altitudes

‒ all directions

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MISSILES AGAINST SRSAM RADARS

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• Reducing range

‒ From: 25 km @ -10 dBm2

‒ To: Range km @ RCS dBm2

• Example:

‒ RCS from hemispherical IR-window = -15 dBm2

• Conclusion:

‒ Cruise missiles are viable candidates for RCS reduction

5 10 15 20

-10

-15

-20

-25

-30

-35

RCS (dBm2)

Range (km)

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RCS OF MISSILES

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MISSILES AGAINST SRSAM RADARS

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• Previous example: -25 dBm2 <=> 10 km detection range

‒ M 3 <=> 10 illuminations by a 1 s surv radar

‒ M 4 <=> 7 illuminations by a 1 s surv radar

• Assume

‒ 2 s response to firing

‒ 30 g acceleration of SA missile

• SA missile hits after

‒ 4.6 s @ 3.2 km range (M 3)

‒ 4.1 s @ 2.5 km range (M 4)

• Conclusions:

‒ close shave, no second chance

‒ jamming + maneuvering can tip balance in cruise missile´s favour

‒ signature management of cruise missiles is meaningful

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MISSILE RADAR ABSORBERS

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• High speed only in terminal phase

‒ M 3-4 is well below plasma formation

• Some fibre composites might work, e.g. cyanate ester / quartz

‒ Tg close to 400 °C

‒ Low e'r and e''r , suitable for EM design

• Topics

‒ edge scattering

‒ grazing incidence

‒ curved surfaces

‒ frontal curvatures relatively small

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MISSILE RADAR ABSORBERS

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• NFFP6: Signature management of low-altitude missiles

‒ Dr C Larsson, Saab Dynamics

‒ Prof D Sjöberg, Lund University

• Problem:

‒ Planar absorber designs are often used for curved surfaces

‒ Absorber capacity degrades

• Highlights:

‒ Resistive layers, magnetic layers, circuit-analog absorbers, bulk loss materials (e.g. doped foams)

‒ Analytical models, full-wave simulations

‒ Bulk loss absorbers generally better than thin-layer designs

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WEAK SPOT

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• Low-frequency radars?

‒ High RCS against current cruise missiles

‒ Would offset signature management

• Normally associated with LR-systems

‒ Poor low-level function

‒ Large <=> Low update rates

‒ Aircraft integration very difficult

• Still: high RCS

‒ Room for innovation!

Az (°)

RCS (dBm2)

0

-180 0 180

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AIRCRAFT RCS APPROACH

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RCS IN FIGHTER COMBAT

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• Keeping everything else equal, the statistical outcome of a duel is noticeably affected by a figure-of-merit, M , that describes one's radar performance relative to one's RCS.

• Simplistically: Largest M wins

• Realistically: M-deficiency can be managed by radar discipline, numbers, tactics, co-operation, performance of other sensors, jammers and links, weapons performance, agility and unpredictability

• But that becomes increasingly harder as dM = M - M increases.

• Conclusion:

‒ Keeping fighter RCS in check is and will be important

2

antoutAPM

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RCS IN FIGHTER COMBAT

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• Cost control by requirement relaxation

• Develop RCS requirement against AEW and fighter radars

• "Spill-over" limits RCS at lower frequencies

‒ higher UHF and upwards

• Develop tactics, EW and armament to handle remaining threats

‒ VHF and lower UHF

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RCS PRICE TAG

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• Cost control by research

• Costs divided into

‒ NRE

‒ Production

‒ Maintenance

• Other penalties

‒ Sensor limitations

‒ Interoperability issues

‒ Weapons load

‒ Availability

• But not

‒ Flight envelope, maneuverability, action radius

0 -5 -10 -15

5C

4C

3C

2C

C

0

NRE (-)

RCS (dBm2)

TRL 5 research base

TRL 1 research base