简氏防务上面的东西权威吗？给大家发一些上面关于兔子装 ...

都是英文，不过数字比较多，应该看得明白。 外文直接复制来的，仅供参考。

1、先是鹰击-12的

Type
Air-to-surface missile (ASM).
Development
An ASM believed to be designated Ying Ji-12 (Eagle Strike-12), was first seen in model form in August 2000, under the centre fuselage of a FBC-1/JH-7 aircraft. The missile was described as anti-ship, anti-radar and with potential for development for land attack.
In 2002 it was seen again, this time on a wing pylon of a FBC-1/JH-7.
Description
The missile is believed to be around 5.0 m long, to have a body diameter of 0.36 m, and a launch weight of 650 kg.
YJ-12
Propulsion
The missile looked similar to the French ASMP, with two rectangular air-inlets each side of the body, four tail control fins, and what is assumed to be a ramjet motor. It is assessed that the YJ-12 uses an integral solid-propellant boost motor, and a liquid-propellant ramjet, with a maximum range of 400 km when cruising at high altitude (15 km) at M2.5. The range at low level would probably be 150 to 200 km. Other sources as yet unconfirmed have quoted the speed of the missile to be up to M4.0

2、然后是歼10的。超大不支持表格，把截图给大家上传了。

3、接下来是鹰击8系列。同样是上传截图。

4、PL12/SD-10.同样是截图。

5、然后是苏27系列的
J-11A:
Designation of Su-27SKs assembled from CKD kits supplied by KnAAPO. Six or seven were planned to be assembled annually during 1999-2001, increasing to 15 to 20 per year from 2002. By late 2004 all 105 parts kits (of diminishing completeness) representing the first batch had been delivered from Russia, of which 60 had been assembled and delivered to PLAAF, but there was no sign of the follow-on order for 95, nor of a change of local manufacture to Su-30MKK variant, as once expected. Acquisition of MKK is now from Russian production. PLA Naval Aviation also received 24 Su-30MK2s in 2004, bringing total 'Flanker' family acquisition to 207.
Completion of the first 105 J-11A kits (all single-seaters, in batches of nine, 24, 24, 24 and 24) was achieved by the end of 2006. (Use of expected JJ-11 designation for two-seaters not taken up: negated by import of 40 Su-27UBKs.) China said to have rejected offer for second batch to be of upgraded Su-27SMK variant, in favour of own J-11B development. According toJane's sources in late 2004, 'several 10s' of J-11As had been refitted under a Russian (Technocomplex group) led programme involving changes to their NIIP N-001 radar to enable them to fire the Vympel RVV-AE (AA-12 'Adder') AAM.
According to one report in September 2007, 15 of original Su-27SK/UBK imports had by then been lost, and only 16 of the remainder were combat-ready at any one time.
J-11B:
Chinese development. Single-seater; as described. Land-based aircraft for PLA Navy may be designated J-11BH.
J-11BS
Tandem-seat (Shuangzuo = two-seat) version reported in 2008; first sighting 2009, of a prototype at CFTE, wearing establishment's serial number 532. This (or another) prototype reported to have crashed at Yanliang in 2009, but BS version said to have been approved by PLAAF in May 2010, with PLA Navy counterpart dubbed J-11BSH. Possibility exists that two-seaters are previous PLAAF Su-27UBKs re-engined with WS10A, but confirmation not yet available.
'J-15'
Purported designation of carrier-based derivative, previously reported as J-11BJ and/or 'J-13'; described separately.
'J-16'
Suggested in mid-2010 as possible designation of long-range strike version of two-seat J-11BS trainer, said to be under development for a first flight in 2011 or 2012. Expected attributes include more powerful radar; fire control system with additional air-to-ground modes; 8,000 kg (17,637 lb) max weapons/stores load, including PL-8/PL-12 AAMs, KD-88 ASMs and LS-500J LGBs; max range of 2,159 n miles (4,000 km; 2,485 miles).
Design Features
Empty weight reduced by about 700 kg (1,543 lb) due to increased use of composites; Chinese-modified Russian engine; Chinese radar and other systems; claimed two-thirds reduction in radar cross-section, achieved by radar wave shield on air intake lips, radar absorbing materials (RAM) on intake interior, and use of signature-reducing paint. Airframe strengthening, achieved via wind tunnel tests of weapons carriage, reportedly extends life to more than 10,000 hours.
Power Plant
Two 132 kN (29,674 lb st) afterburning Liming WS10A Taihang turbofans (Chinese derivative of AL-31FN).
Accommodation
Pilot on 610 Institute TY-8 zero/zero ejection seat.
Avionics
Radar
Indigenous multimode pulse Doppler type, possibly designated Type 1474 or KLJ-4; estimated capability to track 20 targets and simultaneously lock on to six. Domestic electronically scanned array radars expected in 'near future'.

6、歼轰7. 因为数据较多，分两张图片上传

JH7 .jpg (18.1 KB, 下载次数: 5)

下载附件 保存到相册

歼轰7（2）

2013-3-17 12:04 上传

谢谢各位

都是英文，不过数字比较多，应该看得明白。 外文直接复制来的，仅供参考。

1、先是鹰击-12的

Type
Air-to-surface missile (ASM).
Development
An ASM believed to be designated Ying Ji-12 (Eagle Strike-12), was first seen in model form in August 2000, under the centre fuselage of a FBC-1/JH-7 aircraft. The missile was described as anti-ship, anti-radar and with potential for development for land attack.
In 2002 it was seen again, this time on a wing pylon of a FBC-1/JH-7.
Description
The missile is believed to be around 5.0 m long, to have a body diameter of 0.36 m, and a launch weight of 650 kg.
YJ-12
Propulsion
The missile looked similar to the French ASMP, with two rectangular air-inlets each side of the body, four tail control fins, and what is assumed to be a ramjet motor. It is assessed that the YJ-12 uses an integral solid-propellant boost motor, and a liquid-propellant ramjet, with a maximum range of 400 km when cruising at high altitude (15 km) at M2.5. The range at low level would probably be 150 to 200 km. Other sources as yet unconfirmed have quoted the speed of the missile to be up to M4.0

2、然后是歼10的。超大不支持表格，把截图给大家上传了。

3、接下来是鹰击8系列。同样是上传截图。

4、PL12/SD-10.同样是截图。

5、然后是苏27系列的
J-11A:
Designation of Su-27SKs assembled from CKD kits supplied by KnAAPO. Six or seven were planned to be assembled annually during 1999-2001, increasing to 15 to 20 per year from 2002. By late 2004 all 105 parts kits (of diminishing completeness) representing the first batch had been delivered from Russia, of which 60 had been assembled and delivered to PLAAF, but there was no sign of the follow-on order for 95, nor of a change of local manufacture to Su-30MKK variant, as once expected. Acquisition of MKK is now from Russian production. PLA Naval Aviation also received 24 Su-30MK2s in 2004, bringing total 'Flanker' family acquisition to 207.
Completion of the first 105 J-11A kits (all single-seaters, in batches of nine, 24, 24, 24 and 24) was achieved by the end of 2006. (Use of expected JJ-11 designation for two-seaters not taken up: negated by import of 40 Su-27UBKs.) China said to have rejected offer for second batch to be of upgraded Su-27SMK variant, in favour of own J-11B development. According toJane's sources in late 2004, 'several 10s' of J-11As had been refitted under a Russian (Technocomplex group) led programme involving changes to their NIIP N-001 radar to enable them to fire the Vympel RVV-AE (AA-12 'Adder') AAM.
According to one report in September 2007, 15 of original Su-27SK/UBK imports had by then been lost, and only 16 of the remainder were combat-ready at any one time.
J-11B:
Chinese development. Single-seater; as described. Land-based aircraft for PLA Navy may be designated J-11BH.
J-11BS
Tandem-seat (Shuangzuo = two-seat) version reported in 2008; first sighting 2009, of a prototype at CFTE, wearing establishment's serial number 532. This (or another) prototype reported to have crashed at Yanliang in 2009, but BS version said to have been approved by PLAAF in May 2010, with PLA Navy counterpart dubbed J-11BSH. Possibility exists that two-seaters are previous PLAAF Su-27UBKs re-engined with WS10A, but confirmation not yet available.
'J-15'
Purported designation of carrier-based derivative, previously reported as J-11BJ and/or 'J-13'; described separately.
'J-16'
Suggested in mid-2010 as possible designation of long-range strike version of two-seat J-11BS trainer, said to be under development for a first flight in 2011 or 2012. Expected attributes include more powerful radar; fire control system with additional air-to-ground modes; 8,000 kg (17,637 lb) max weapons/stores load, including PL-8/PL-12 AAMs, KD-88 ASMs and LS-500J LGBs; max range of 2,159 n miles (4,000 km; 2,485 miles).
Design Features
Empty weight reduced by about 700 kg (1,543 lb) due to increased use of composites; Chinese-modified Russian engine; Chinese radar and other systems; claimed two-thirds reduction in radar cross-section, achieved by radar wave shield on air intake lips, radar absorbing materials (RAM) on intake interior, and use of signature-reducing paint. Airframe strengthening, achieved via wind tunnel tests of weapons carriage, reportedly extends life to more than 10,000 hours.
Power Plant
Two 132 kN (29,674 lb st) afterburning Liming WS10A Taihang turbofans (Chinese derivative of AL-31FN).
Accommodation
Pilot on 610 Institute TY-8 zero/zero ejection seat.
Avionics
Radar
Indigenous multimode pulse Doppler type, possibly designated Type 1474 or KLJ-4; estimated capability to track 20 targets and simultaneously lock on to six. Domestic electronically scanned array radars expected in 'near future'.

6、歼轰7. 因为数据较多，分两张图片上传

JH7 .jpg (18.1 KB, 下载次数: 5)

下载附件 保存到相册

歼轰7（2）

2013-3-17 12:04 上传

谢谢各位