S-A-B-E-R->
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thats a twin seater just like F16 b or d so the spine to accomodate the equipment moved back i think
Chengdu J-10 Multirole Fighter Air Craft News & Discussions
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SBD-3
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I think they are trying to make up for it by using Multi Rail Launchers mounted underwing, but I do agree that there could be a wingtip rail for WVRs.
krash
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Yes S-A-B-E-R is correct you'll only see the spine on the 'S' version i.e. the duel seater. Post 4947 shows a duel seater while the one in post 4948 is a single seater.
Mani2020
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The spine is there in double seater versions to made up for the room occupied by housing the second seat , so a spine is needed to house the electronic stuff which otherwise would have been in place of second seat in single seat version. This spine is also available on PAF's F-16 block 52+ D version
Yodhashakti
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Any update regarding the aircraft ?
When will the delivery begin ?
When will the delivery begin ?
AZADPAKISTAN2009
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No rush , we are not in hurry its not like we are going to war with our neighbors but we plan to induct 2014 while retiring bunch of old planes
epinephrine
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india-pak relations r very fragile.a single blast on indian soil by some terrorists is sufficient enough to bring the armies of both countries on the border.
fatman17
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J-10/10A Vigorous Dragon - update
A PLAAF J-10A was photographed while carrying training rounds of PL-8 and PL-12 AAMs. J-10 (K/JJ10?) is a multi-functional single-engine fighter being developed by Chengdu Aircraft Corporation (CAC) and 611 Institute. It has been selected by PLAAF as the next generation fighter to replace the obsolete J-7 fighter and Q-5 attack aircraft. The aircraft appears to have an Su-27 style nose and rectangular air intake, an AL-31F type engine, twin nose wheels, and a distinct low-visibility camouflage color scheme. The aircraft also has a large vertical tail plus twin F-16 style ventral stabilizers believed to provide greater stability at high AoA. Its fuselage looks considerably longer compared to Israeli Lavi. Unlike J-7E with double-delta wings, it appears to have a pair of inverted gull wings (i.e. the inner upper portion extends slightly downward, while the outer portion extends flat). Two red dummy PL-8 AAMs have been regularly seen carried under the wing as well. The J-10 project was conceived in the 1984 based on the experience (tailless delta wing and canard foreplanes) with J-9 which was cancelled in 1980 in favor of the less risky J-7C/MIG-21MF project. An early model of J-10 revealed a Mirage 2000 style intake with a center shock cone for better high speed performance and a Lavi style tail section, suggesting a possible connection with the cancelled Israeli fighter (however this was firmly denied by both parties). The change indicates that J-10 has gone through at least one major redesign in its 18-year development period from the initial conventional layout as an air-superiority fighter to the latest semi-stealthy design as a multi-role fighter. This change may reflect a shift of its potential adversaries from former Soviet Mig-29/Su-27 to current American F-15/16/18 after end of the Cold War. The new design is certainly fitted with advanced avionics including a "glass cockpit" (1 wide-angle HUD + 2 monochrome MFD + 1 color MFD), HMS, HOTAS, GPS/INS, air data computer, ARW9101A RWR, Type 634 digital quadruplex FBW, digital fuel management system, mission management system, 1553B databus, and a detachable IFR probe. A new PD fire-control radar (Type 1473? search >120km, track 4-6, engage 2 simultaneously) is also fitted, but the exact designation is still unknown. A variety of newly developed air-to-air (e.g. PL-8 short-range IR guided AAM and PL-12 medium-range active radar guided AAM) and air-to-surface weapons including KD-88 TV guided ASMs and LS-500J LGBs are also expected to be carried under 11 hardpoints. A new twin-rail missile launch pylon was developed to increase the total number of PL-12 MRAAMs it can carry from 2 to 4. Although it was believed to be powered initially by a 27,560lb/12,500kg thrust AL-31FN turbofan, a modified AL-31F which itself powers Su-27/J-11, Russia reportedly had denied China the license to produce the engine locally. As the result, an indigenous engine (WS-10A) may be fitted later in the serial production. Some US military analysts believed that J-10 could pose a serious challenge to F/A-18E in terms of maneuverability. Some specifications of J-10 are (estimated): empty weight 9,750kg, max TO weight 19,277kg, internal fuel 4,500kg, external load 4,500kg, g load +9/-3, max speed Mach 2.0 (high altitude)/Mach 1.2 (1,450km/h @ sea level), TO distance <500m, combat radius 1,100km, dynamic ceiling 20,300m, ferry range 3,200km. The development of J-10 has not been smooth. A full-scale mock-up was built in 1991. The first prototype was set to fly in 1996, powered by a newly developed WS-10 turbofan based on the CFM56 engine core technology. However the development of this indigenous engine suffered serious difficulties and thus the rear fuselage and engine intake were forced to be redesigned in order to accommodate an alternative AL-31FN engine imported from Russia. After a 15-month delay, the first prototype (01/1001) was rolled out in June 1997. It made its maiden flight on March 23, 1998, two years behind the schedule. 6 prototypes (serial numbers 1002-1009) were built undergoing various static and flight tests at CAC in Chengdu and at the CFTE in Yanliang. Subsequently 3 more prototypes were built (1013-1016) as the project was moving into the pre-production phase while PLAAF remained fully committed. The flight test of J-10 was completed by the end of 2003 and the serial production started earlier that year. Approximately two are being produced each month. A total of 300 have been planned. The first J-10 in production standard first flew on June 28, 2002. The initial batches of 50 (54 AL-31FNs were imported between 2002 and 2004) have been produced by CAC, wearing a new gray/light blue paint scheme. Currently the production continues at a rate of 2-3 per month. This rate may increase when the 2nd assembly line is established. The first 9 (?) were delivered to the PLAAF Flight Test & Training Base for evaluation starting from February 2003 (S/N 60x8x). After some delay due the problems of fire-control system, J-10 was finally certified by the end of 2003. The first J-10 regiment was established in 2004 in the PLAAF 44th Division stationed in Yunnan Province facing India. Around 100 may have been produced by 2006 (01-03 batch, S/N 50x5x, 10x4x, 10x3x, 10x2x, 20x0x). J-10 was officially declassified on December 29, 2006. Some improvements have been made during the production, including a WL-9 radio compass antenna dish behind the canopy. A tandem-seat trainer/attack version (J-10S) has been developed too (see below). Further improved variants including J-10A (improved glass cockpit) and J-10B (JF-17 style cockpit, IRST/LR, AESA radar, DSI engine intake, RAM coating) have been developed (see below). An export version (dubbed FC-20?) is also under development. Its first customer is likely to be Pakistan. Currently J-10A is entering the service with PLAAF (04 batch, S/N 50x5x, 30x5x, 60x8x). The August 1 Aerobatic Demonstration Team also flies J-10AY (05 batch) to replace the old J-7GB. The latest image confirmed that PLAN is receiving its first batch of J-10As (06 batch? dubbed J-10AH? S/N 83x4x).
- Last Updated 9/11/11
J-10S Vigorous Dragon - update
A PLAAF 44th Division J-10S (JJ-10?) advanced trainer was taking off. This version features a stretched forward fuselage and a bubble canopy which can be opened as a single piece. An excellent 360° outside view in the rear cockpit is clearly shown in the photo. Its dorsal spine appears to have been enlarged to accommodate electronics displaced by the rear cockpit. In addition to being a trainer for J-10 pilots, J-10S is likely to be converted into an attack aircraft or EW/Wild Weasel anti-radiation aircraft, where it might carry Blue Sky low altitude navigation pod (similar to American LANTIRN pod), laser designation pod, as well as LS-500J LGBs and KD-88 ASMs. First Flight of 01 prototype took place on December 26, 2003. Two prototypes (01/1021 & 03/1023) were built undergoing various flight tests. J-10S passed the state certification in late 2005 and has entered service with PLAAF (S/N 10x4x, 50x5x, 10x3x, 60x8x). In addition, the August 1 Aerobatic Demonstration Team has been flying J-10SY since mid-2010. In late 2010 the first batch of J-10Ss are entering the service with PLAN (dubbed J-10SH? S/N 83x4x) along with J-10As.
- Last Updated 7/24/11
J-10B Vigorous Dragon - update
The latest 1035 prototype of the J-10B was photographed at CAC airfield in July 2011, revealing the indigenous WS-10B (?) turbofan engine. This much improved variant (1031 prototype) made its maiden flight on December 23, 2008, powered by a Russian AL-31FN engine. The improvements include a DSI/bump engine inlet which not only cuts weight but also reduces RCS, after a similar design was first tested onboard FC-1/JF-17. The aircraft also features a J-11B style IRST/LR and a wide-angle holographic HUD. IRST enables passive detection of enemy aircraft, making J-10B more stealthy in combat. Its nose appears flatter too, similar to that of American F-16, and fire-control radar is thought to be an X-band AESA developed by the 14th Institute, the first of such type ever being developed for a Chinese fighter aircraft, giving J-10B a stronger multi-target engagement and ECCM capability. Two large pods housing testing equipments are attached under the wings. The tip of vertical tailfin was redesigned as well, featuring a large fairing containing communication and ECM antennas, which resembles that of French Mirage 2000. A rear facing MAWS sensor can be seen underneath the parachute boom. A similar system was tested onboard FC-1/JF-17. RAM coating is also expected in certain areas such as engine inlet and wing leading edges to reduce RCS. The aircraft may be fitted with CFTs in the future to further extend its range. All these improvements suggest that J-10B is equipped with a new generation of integrated electronic system, ranging from radar to EW system. Its mission may be changed from air-superiority to multi-role, such as CAS or EW. For air-superiority mission, normally 6 AAMs (PL-12x4 + PL-8x2, PL-12s are carried underneath the twin-rail launch pylon) can be carried. For CAS mission, normally 2 KD-88 AGMs or LS-500J LGBs can be carried. In addition, the aircraft is expected to be powered eventually by a WS-10B turbofan. Overall J-10B is thought to be comparable to American F-16E/Block 60. The 03 prototype first flew in August 2009, with the pitot tube removed from the nose tip. Both 1031 & 1034 prototypes are currently being tested at CFTE. J-10B is very likely to serve as a testbed for various advanced technologies adopted by the 4th generation J-20 (see below) currently under development at CAC thus may not enter the service in large quantity with PLAAF. The production of J-10B is expected to be imminent (07 batch?).
- Last Updated 9/7/11
A PLAAF J-10A was photographed while carrying training rounds of PL-8 and PL-12 AAMs. J-10 (K/JJ10?) is a multi-functional single-engine fighter being developed by Chengdu Aircraft Corporation (CAC) and 611 Institute. It has been selected by PLAAF as the next generation fighter to replace the obsolete J-7 fighter and Q-5 attack aircraft. The aircraft appears to have an Su-27 style nose and rectangular air intake, an AL-31F type engine, twin nose wheels, and a distinct low-visibility camouflage color scheme. The aircraft also has a large vertical tail plus twin F-16 style ventral stabilizers believed to provide greater stability at high AoA. Its fuselage looks considerably longer compared to Israeli Lavi. Unlike J-7E with double-delta wings, it appears to have a pair of inverted gull wings (i.e. the inner upper portion extends slightly downward, while the outer portion extends flat). Two red dummy PL-8 AAMs have been regularly seen carried under the wing as well. The J-10 project was conceived in the 1984 based on the experience (tailless delta wing and canard foreplanes) with J-9 which was cancelled in 1980 in favor of the less risky J-7C/MIG-21MF project. An early model of J-10 revealed a Mirage 2000 style intake with a center shock cone for better high speed performance and a Lavi style tail section, suggesting a possible connection with the cancelled Israeli fighter (however this was firmly denied by both parties). The change indicates that J-10 has gone through at least one major redesign in its 18-year development period from the initial conventional layout as an air-superiority fighter to the latest semi-stealthy design as a multi-role fighter. This change may reflect a shift of its potential adversaries from former Soviet Mig-29/Su-27 to current American F-15/16/18 after end of the Cold War. The new design is certainly fitted with advanced avionics including a "glass cockpit" (1 wide-angle HUD + 2 monochrome MFD + 1 color MFD), HMS, HOTAS, GPS/INS, air data computer, ARW9101A RWR, Type 634 digital quadruplex FBW, digital fuel management system, mission management system, 1553B databus, and a detachable IFR probe. A new PD fire-control radar (Type 1473? search >120km, track 4-6, engage 2 simultaneously) is also fitted, but the exact designation is still unknown. A variety of newly developed air-to-air (e.g. PL-8 short-range IR guided AAM and PL-12 medium-range active radar guided AAM) and air-to-surface weapons including KD-88 TV guided ASMs and LS-500J LGBs are also expected to be carried under 11 hardpoints. A new twin-rail missile launch pylon was developed to increase the total number of PL-12 MRAAMs it can carry from 2 to 4. Although it was believed to be powered initially by a 27,560lb/12,500kg thrust AL-31FN turbofan, a modified AL-31F which itself powers Su-27/J-11, Russia reportedly had denied China the license to produce the engine locally. As the result, an indigenous engine (WS-10A) may be fitted later in the serial production. Some US military analysts believed that J-10 could pose a serious challenge to F/A-18E in terms of maneuverability. Some specifications of J-10 are (estimated): empty weight 9,750kg, max TO weight 19,277kg, internal fuel 4,500kg, external load 4,500kg, g load +9/-3, max speed Mach 2.0 (high altitude)/Mach 1.2 (1,450km/h @ sea level), TO distance <500m, combat radius 1,100km, dynamic ceiling 20,300m, ferry range 3,200km. The development of J-10 has not been smooth. A full-scale mock-up was built in 1991. The first prototype was set to fly in 1996, powered by a newly developed WS-10 turbofan based on the CFM56 engine core technology. However the development of this indigenous engine suffered serious difficulties and thus the rear fuselage and engine intake were forced to be redesigned in order to accommodate an alternative AL-31FN engine imported from Russia. After a 15-month delay, the first prototype (01/1001) was rolled out in June 1997. It made its maiden flight on March 23, 1998, two years behind the schedule. 6 prototypes (serial numbers 1002-1009) were built undergoing various static and flight tests at CAC in Chengdu and at the CFTE in Yanliang. Subsequently 3 more prototypes were built (1013-1016) as the project was moving into the pre-production phase while PLAAF remained fully committed. The flight test of J-10 was completed by the end of 2003 and the serial production started earlier that year. Approximately two are being produced each month. A total of 300 have been planned. The first J-10 in production standard first flew on June 28, 2002. The initial batches of 50 (54 AL-31FNs were imported between 2002 and 2004) have been produced by CAC, wearing a new gray/light blue paint scheme. Currently the production continues at a rate of 2-3 per month. This rate may increase when the 2nd assembly line is established. The first 9 (?) were delivered to the PLAAF Flight Test & Training Base for evaluation starting from February 2003 (S/N 60x8x). After some delay due the problems of fire-control system, J-10 was finally certified by the end of 2003. The first J-10 regiment was established in 2004 in the PLAAF 44th Division stationed in Yunnan Province facing India. Around 100 may have been produced by 2006 (01-03 batch, S/N 50x5x, 10x4x, 10x3x, 10x2x, 20x0x). J-10 was officially declassified on December 29, 2006. Some improvements have been made during the production, including a WL-9 radio compass antenna dish behind the canopy. A tandem-seat trainer/attack version (J-10S) has been developed too (see below). Further improved variants including J-10A (improved glass cockpit) and J-10B (JF-17 style cockpit, IRST/LR, AESA radar, DSI engine intake, RAM coating) have been developed (see below). An export version (dubbed FC-20?) is also under development. Its first customer is likely to be Pakistan. Currently J-10A is entering the service with PLAAF (04 batch, S/N 50x5x, 30x5x, 60x8x). The August 1 Aerobatic Demonstration Team also flies J-10AY (05 batch) to replace the old J-7GB. The latest image confirmed that PLAN is receiving its first batch of J-10As (06 batch? dubbed J-10AH? S/N 83x4x).
- Last Updated 9/11/11
J-10S Vigorous Dragon - update
A PLAAF 44th Division J-10S (JJ-10?) advanced trainer was taking off. This version features a stretched forward fuselage and a bubble canopy which can be opened as a single piece. An excellent 360° outside view in the rear cockpit is clearly shown in the photo. Its dorsal spine appears to have been enlarged to accommodate electronics displaced by the rear cockpit. In addition to being a trainer for J-10 pilots, J-10S is likely to be converted into an attack aircraft or EW/Wild Weasel anti-radiation aircraft, where it might carry Blue Sky low altitude navigation pod (similar to American LANTIRN pod), laser designation pod, as well as LS-500J LGBs and KD-88 ASMs. First Flight of 01 prototype took place on December 26, 2003. Two prototypes (01/1021 & 03/1023) were built undergoing various flight tests. J-10S passed the state certification in late 2005 and has entered service with PLAAF (S/N 10x4x, 50x5x, 10x3x, 60x8x). In addition, the August 1 Aerobatic Demonstration Team has been flying J-10SY since mid-2010. In late 2010 the first batch of J-10Ss are entering the service with PLAN (dubbed J-10SH? S/N 83x4x) along with J-10As.
- Last Updated 7/24/11
J-10B Vigorous Dragon - update
The latest 1035 prototype of the J-10B was photographed at CAC airfield in July 2011, revealing the indigenous WS-10B (?) turbofan engine. This much improved variant (1031 prototype) made its maiden flight on December 23, 2008, powered by a Russian AL-31FN engine. The improvements include a DSI/bump engine inlet which not only cuts weight but also reduces RCS, after a similar design was first tested onboard FC-1/JF-17. The aircraft also features a J-11B style IRST/LR and a wide-angle holographic HUD. IRST enables passive detection of enemy aircraft, making J-10B more stealthy in combat. Its nose appears flatter too, similar to that of American F-16, and fire-control radar is thought to be an X-band AESA developed by the 14th Institute, the first of such type ever being developed for a Chinese fighter aircraft, giving J-10B a stronger multi-target engagement and ECCM capability. Two large pods housing testing equipments are attached under the wings. The tip of vertical tailfin was redesigned as well, featuring a large fairing containing communication and ECM antennas, which resembles that of French Mirage 2000. A rear facing MAWS sensor can be seen underneath the parachute boom. A similar system was tested onboard FC-1/JF-17. RAM coating is also expected in certain areas such as engine inlet and wing leading edges to reduce RCS. The aircraft may be fitted with CFTs in the future to further extend its range. All these improvements suggest that J-10B is equipped with a new generation of integrated electronic system, ranging from radar to EW system. Its mission may be changed from air-superiority to multi-role, such as CAS or EW. For air-superiority mission, normally 6 AAMs (PL-12x4 + PL-8x2, PL-12s are carried underneath the twin-rail launch pylon) can be carried. For CAS mission, normally 2 KD-88 AGMs or LS-500J LGBs can be carried. In addition, the aircraft is expected to be powered eventually by a WS-10B turbofan. Overall J-10B is thought to be comparable to American F-16E/Block 60. The 03 prototype first flew in August 2009, with the pitot tube removed from the nose tip. Both 1031 & 1034 prototypes are currently being tested at CFTE. J-10B is very likely to serve as a testbed for various advanced technologies adopted by the 4th generation J-20 (see below) currently under development at CAC thus may not enter the service in large quantity with PLAAF. The production of J-10B is expected to be imminent (07 batch?).
- Last Updated 9/7/11
Chinas J-10B fighter to Pak worries India - India - DNA
Chinas J-10B fighter to Pak worries India
Published: Thursday, Aug 4, 2011, 15:26 IST
By Hemanth CS | Place: Bangalore | Agency: DNA
The recent official offer of the Chinese to raise a squadron of its home-grown advanced multi-role, all-weather fighter aircraft J-10B to Pakistan has worried Indian defence experts. Pakistan will be the only other country apart from China to have this sophisticated fighter aircraft.
Air Commodore (Retd) Jasjit Singh, director, New Delhi-based Centre for Air Power Studies (CAPS), told DNA: India now not only faces the possibility of a two-front war but has to also deal with a two-front military modernisation programme with China supplying its latest weaponry to Pakistan.
He said India faces a 10-year window of vulnerability as the Indian Air Forces (IAFs) present squadron of 34 is way below the sanctioned strength of 39 squadrons. It will take 10 years for the IAF to get back to its sanctioned strength of 39 squadrons. While Pakistan at present, with 24 squadrons, is raising its strength rapidly with Chinas support, said Singh, who is also the former director of Institute for Defence Studies and Analysis.
Former Vice Chief of Air Staff, Air Marshal PK Barbora, however, said Chinas offering Pakistan a squadron of the J-10s may not threaten Indias air superiority. China does not have a great record of producing a world-class aircraft. All they do is reverse engineer and manufacture aircraft. Secondly, by raising just one squadron Pakistan may not benefit much, he said.
However, Pakistani media reports indicate that it is looking at raising two squadrons of the fourth generation aircraft to counter Indias Light Combat Aircraft (LCA) Tejas, which is still under development. Besides, according to US military and defence technology news website, Defense Update, the Chinese designed Joint Fighter (JF)-17 (commonly known as Thunder) is already under production in Pakistan and is actively being promoted for export in the world market.
Despite his optimism, Air Marshal Barbora warned that the slow pace of Indias defence indigenisation (read LCA Tejas, in particular) is a cause for worry. We will be adding 300 more Su-30 MKIs; getting 126 medium multi role combat aircraft; and upgrading the Mirage 2000s, Jaguars and the MiG-29s. The same cannot be said of some pathetic status of indigenous programmes like the Light Combat Aircraft, which has been delayed for years now, he says.
Chinas J-10B fighter to Pak worries India
Published: Thursday, Aug 4, 2011, 15:26 IST
By Hemanth CS | Place: Bangalore | Agency: DNA
The recent official offer of the Chinese to raise a squadron of its home-grown advanced multi-role, all-weather fighter aircraft J-10B to Pakistan has worried Indian defence experts. Pakistan will be the only other country apart from China to have this sophisticated fighter aircraft.
Air Commodore (Retd) Jasjit Singh, director, New Delhi-based Centre for Air Power Studies (CAPS), told DNA: India now not only faces the possibility of a two-front war but has to also deal with a two-front military modernisation programme with China supplying its latest weaponry to Pakistan.
He said India faces a 10-year window of vulnerability as the Indian Air Forces (IAFs) present squadron of 34 is way below the sanctioned strength of 39 squadrons. It will take 10 years for the IAF to get back to its sanctioned strength of 39 squadrons. While Pakistan at present, with 24 squadrons, is raising its strength rapidly with Chinas support, said Singh, who is also the former director of Institute for Defence Studies and Analysis.
Former Vice Chief of Air Staff, Air Marshal PK Barbora, however, said Chinas offering Pakistan a squadron of the J-10s may not threaten Indias air superiority. China does not have a great record of producing a world-class aircraft. All they do is reverse engineer and manufacture aircraft. Secondly, by raising just one squadron Pakistan may not benefit much, he said.
However, Pakistani media reports indicate that it is looking at raising two squadrons of the fourth generation aircraft to counter Indias Light Combat Aircraft (LCA) Tejas, which is still under development. Besides, according to US military and defence technology news website, Defense Update, the Chinese designed Joint Fighter (JF)-17 (commonly known as Thunder) is already under production in Pakistan and is actively being promoted for export in the world market.
Despite his optimism, Air Marshal Barbora warned that the slow pace of Indias defence indigenisation (read LCA Tejas, in particular) is a cause for worry. We will be adding 300 more Su-30 MKIs; getting 126 medium multi role combat aircraft; and upgrading the Mirage 2000s, Jaguars and the MiG-29s. The same cannot be said of some pathetic status of indigenous programmes like the Light Combat Aircraft, which has been delayed for years now, he says.
Fieldmarshal
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All credibility in the article was lost when the author penned the following lines 'looking at raising two squadrons of the fourth generation aircraft to counter Indias Light Combat Aircraft (LCA) Tejas, which is still under development' .
india needs to field the lca first for PAF to "counter it" with a ft-5 let alone a third gen ac.
If 300 mki and couple of hundred upgraded mig29, mirage 2000 and jaguars cant deal with the threat and u need a failure of an a/c (LCA) than it surely points towards a deep inferiority complex and a sense of insecurity.
Guess the 1000 years of Muslim rule has done u in for life.
Black Widow
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So you too believe this bed-time story??? Rest of your comments are un-answerable...
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