C803的空射型射程高达400km？

SALSCM

An advanced successor of C-803 is underdevelopment by China Aviation Industry Corporation I, and this follow-on of C-803 was first revealed at the 6th Zhuhai Airshow in 2006, shown in model form carried by Xian JH-7. SALSCM stands for Standoff Air-Launched Supersonic Cruise Missile, which is drawn heavily on Russian expertise, but sources differ on how the foreign help was obtained. According to western intelligence, a complete nuclear air-to-surface missile production facility was sold to China in 1995, and this missile production facility was used to manufacture Kh-55/65/RKV-500/AS-15, Kh-15/AS-16 & Kh-31/AS-17.[2] Many Chinese internet sources, however, claim that the foreign help was much more to do with China hiring Russian and Ukrainian missile experts of AS-15/16/17 missile programs after the collapse of former USSR, and China Haiying Electromechanical Technology Academy is one of the top three Chinese missile developing establishment that received former Soviet missile experts.
The heavy Russian influence of SALSCM is obviously reflected in the flight pass during its attack on target: after launching, the missile would first climb up to high level cruise altitude where it turns into level flight, and at the last moment, it dives down on its target, exactly like the way Kh-15/AS-16 AShM does.[3] The same practice is also adopted on anther Chinese AShM YJ-12, which like SALSCM, can also be used against land targets in addition to ships.[4] SALSCM looks like an enlarged C-803, but the control surfaces of the missile closely resembles Russian Kh-35, and a rectangular intake is under the fuselage, and two can be carried by JH-7, though other platforms such as Xian H-6 can also deploy the weapon.[5] Specifications of SALSCM:
Length: 4.18 m
Diameter: 0.56 m
Weight: 980 kg
Warhead: 300 kg
Minimum launching altitude: 10 km
Maximum launching altitude: 20 km
Minimum launching speed: 0.8 Mach
Maximum launching speed: 1.5 Mach
Cruise altitude: 10 to 20 km
Range: 400 km max
Mid course guidance: combined inertial navigation + satellite navigation
Terminal guidance: Combined active millimeter wave radar + imaging infraredSALSCM

An advanced successor of C-803 is underdevelopment by China Aviation Industry Corporation I, and this follow-on of C-803 was first revealed at the 6th Zhuhai Airshow in 2006, shown in model form carried by Xian JH-7. SALSCM stands for Standoff Air-Launched Supersonic Cruise Missile, which is drawn heavily on Russian expertise, but sources differ on how the foreign help was obtained. According to western intelligence, a complete nuclear air-to-surface missile production facility was sold to China in 1995, and this missile production facility was used to manufacture Kh-55/65/RKV-500/AS-15, Kh-15/AS-16 & Kh-31/AS-17.[2] Many Chinese internet sources, however, claim that the foreign help was much more to do with China hiring Russian and Ukrainian missile experts of AS-15/16/17 missile programs after the collapse of former USSR, and China Haiying Electromechanical Technology Academy is one of the top three Chinese missile developing establishment that received former Soviet missile experts.
The heavy Russian influence of SALSCM is obviously reflected in the flight pass during its attack on target: after launching, the missile would first climb up to high level cruise altitude where it turns into level flight, and at the last moment, it dives down on its target, exactly like the way Kh-15/AS-16 AShM does.[3] The same practice is also adopted on anther Chinese AShM YJ-12, which like SALSCM, can also be used against land targets in addition to ships.[4] SALSCM looks like an enlarged C-803, but the control surfaces of the missile closely resembles Russian Kh-35, and a rectangular intake is under the fuselage, and two can be carried by JH-7, though other platforms such as Xian H-6 can also deploy the weapon.[5] Specifications of SALSCM:
Length: 4.18 m
Diameter: 0.56 m
Weight: 980 kg
Warhead: 300 kg
Minimum launching altitude: 10 km
Maximum launching altitude: 20 km
Minimum launching speed: 0.8 Mach
Maximum launching speed: 1.5 Mach
Cruise altitude: 10 to 20 km
Range: 400 km max
Mid course guidance: combined inertial navigation + satellite navigation
Terminal guidance: Combined active millimeter wave radar + imaging infrared