Radar:
Below is my assessment of the inferiority of the CAPTOR vs more modern technologies and the adverse effects on the Typhoons.
In the next few years there will be a number of upgrades to the systems software till Final Operational Capability is attained. Following this a number of hardware upgrades are planned. These involve changing a number of both the shop replaceable items and line replaceable units. These upgrades will focus on improving resolution and ECCM capabilities. The next upgrades will see a switchover to off-the-shelf components. Even with these improvements there are a number of fundamental weaknesses in the CAPTOR's design such as; relatively slow scanning speeds compared to newer technology arrays, relative ease of detection, effects on RCS, etc.
Source:
http://www.eurofighter-typhoon.co.uk/Eurofighter/sensors.html
-Acknowledgement of RELATIVE slow scanning speed compared to AESA/ESA
-Ease of Detection when in operation
-Adversely affects the RCS of the aircraft
-Vulnerable to jamming
-Cost, both maintenance and procurement
-Improved resolution. A vague statement but probably in regard to NCTR or ground mapping/target aquisition
-Limited ability to interleave modes of operation and simultaneous target processing
These flaws will take extensive redesign and/or a different radar altogether to correct. Not a small task and very significant indeed. In my opinion this is perhaps one of the most significant weakness of the Typhoon when compared to other fighters of the 3rd or 4th generation equipped with AESA/ESA radars.
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SUPERCRUISE:
Definitions, discriptions and graph:
http://www.centennialofflight.gov/essay/Theories_of_Flight/Transonic_Flow/TH19.htm
http://en.wikipedia.org/wiki/Supersonic
http://roland.lerc.nasa.gov/~dglover/dictionary/content.html
http://roland.lerc.nasa.gov/~dglover/dictionary/t.html
http://en.wikipedia.org/wiki/Transonic
http://aerodyn.org/Drag/Gifs/drag_rise.gif
EADs and Eurojet claim supercruise at M1.2-M1.3(depending probably on external config) which is clearly in the TRANSONIC region. A futher claim suggest an engine upgrade to allow M1.5 but configuration is unspecified. So to settle the long long standing dispute the Eurofigher DOES NOT SUPERCRUISE. Disagreement with this point, not that there should be any, should focus on SUPERCRUISE rather than exceeding Mach 1 which is what the Eurofigher has demonstrated. SUPERSONIC being defines as ALL AIRFLOW AROUND THE AIRFRAME being supersonic. Also consider that the configuration typically discussed has 50% fuel load which doesnt bode very well when you factor in the SFC ~23g/kn at max military power. Also the claimed Eurofighter supercruise capability originates for a 1998 WAP Journal Volume 35 Winter 1998 edition. The 44 page article describes how a Eurofighter flying at 40,000ft with 6 mock up air to air missiles and 50% fuel load ACCELERATES TO M1.4 WITH AFTERBURNER during a supersonic acceleration test. After which the pilot disengaged the after burner and the aircraft decelerated to about M1.0~M1.1 and held that speed briefly without the afterburner on.
FYI-
F-14/15/16/18
F-104
EE
Draken and some Migs/SUs
Rafale
All of the above can fly just above Mach 1 in military power again depending on configuration and have been able to do so for decades. So NOTHING IS NEW OR REVOLUTIONARY about the Eurofighter false claim of supercruise.
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Cost:
20 billion pounds for the RAF program cost!!!
****************************************************************************
Schedule:
5 years late if we accept the sub standard Tranche 1 IOC. Longer(10 years) for the Tranche 2+.
****************************************************************************
Relevence:
Considering the limited air to ground capability vs comparable types. I would include this as one of the detractions of the type but not always because some users have different requirements. But still considering the price and the ability of Other 4th Gen designs like the F-16 Block 60, Gripen and others it has to be a factor.
Below is my assessment of the inferiority of the CAPTOR vs more modern technologies and the adverse effects on the Typhoons.
In the next few years there will be a number of upgrades to the systems software till Final Operational Capability is attained. Following this a number of hardware upgrades are planned. These involve changing a number of both the shop replaceable items and line replaceable units. These upgrades will focus on improving resolution and ECCM capabilities. The next upgrades will see a switchover to off-the-shelf components. Even with these improvements there are a number of fundamental weaknesses in the CAPTOR's design such as; relatively slow scanning speeds compared to newer technology arrays, relative ease of detection, effects on RCS, etc.
Source:
http://www.eurofighter-typhoon.co.uk/Eurofighter/sensors.html
-Acknowledgement of RELATIVE slow scanning speed compared to AESA/ESA
-Ease of Detection when in operation
-Adversely affects the RCS of the aircraft
-Vulnerable to jamming
-Cost, both maintenance and procurement
-Improved resolution. A vague statement but probably in regard to NCTR or ground mapping/target aquisition
-Limited ability to interleave modes of operation and simultaneous target processing
These flaws will take extensive redesign and/or a different radar altogether to correct. Not a small task and very significant indeed. In my opinion this is perhaps one of the most significant weakness of the Typhoon when compared to other fighters of the 3rd or 4th generation equipped with AESA/ESA radars.
****************************************************************************
SUPERCRUISE:
Definitions, discriptions and graph:
http://www.centennialofflight.gov/essay/Theories_of_Flight/Transonic_Flow/TH19.htm
http://en.wikipedia.org/wiki/Supersonic
http://roland.lerc.nasa.gov/~dglover/dictionary/content.html
http://roland.lerc.nasa.gov/~dglover/dictionary/t.html
http://en.wikipedia.org/wiki/Transonic
http://aerodyn.org/Drag/Gifs/drag_rise.gif
EADs and Eurojet claim supercruise at M1.2-M1.3(depending probably on external config) which is clearly in the TRANSONIC region. A futher claim suggest an engine upgrade to allow M1.5 but configuration is unspecified. So to settle the long long standing dispute the Eurofigher DOES NOT SUPERCRUISE. Disagreement with this point, not that there should be any, should focus on SUPERCRUISE rather than exceeding Mach 1 which is what the Eurofigher has demonstrated. SUPERSONIC being defines as ALL AIRFLOW AROUND THE AIRFRAME being supersonic. Also consider that the configuration typically discussed has 50% fuel load which doesnt bode very well when you factor in the SFC ~23g/kn at max military power. Also the claimed Eurofighter supercruise capability originates for a 1998 WAP Journal Volume 35 Winter 1998 edition. The 44 page article describes how a Eurofighter flying at 40,000ft with 6 mock up air to air missiles and 50% fuel load ACCELERATES TO M1.4 WITH AFTERBURNER during a supersonic acceleration test. After which the pilot disengaged the after burner and the aircraft decelerated to about M1.0~M1.1 and held that speed briefly without the afterburner on.
FYI-
F-14/15/16/18
F-104
EE
Draken and some Migs/SUs
Rafale
All of the above can fly just above Mach 1 in military power again depending on configuration and have been able to do so for decades. So NOTHING IS NEW OR REVOLUTIONARY about the Eurofighter false claim of supercruise.
****************************************************************************
Cost:
20 billion pounds for the RAF program cost!!!
****************************************************************************
Schedule:
5 years late if we accept the sub standard Tranche 1 IOC. Longer(10 years) for the Tranche 2+.
****************************************************************************
Relevence:
Considering the limited air to ground capability vs comparable types. I would include this as one of the detractions of the type but not always because some users have different requirements. But still considering the price and the ability of Other 4th Gen designs like the F-16 Block 60, Gripen and others it has to be a factor.
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