I WILL FIRST START WITH THE BEST OF THE BEST.
The AGM-158 ( used on B-52H, F-16C/D, F/A-18E/F, F-15E, F-117, B-1B, B-2, P-3C and S-3B) weapon is required to attack both fixed and relocatable targets at ranges beyond enemy air defenses and incorporates a high degree of stealth to improve its ability to penetrate enemy air defenses(more than 200 miles with a ER v. at 500 miles). After launch, it will be able to fly autonomously over a low-level, circuitous route to the area of a target, where an autonomous terminal guidance system will guide the missile in for a direct hit.
The key performance parameters for the system are Missile Mission Effectiveness, range, and carrier operability.
JASSM's midcourse guidance is provided by a Global Positioning System (GPS)-aided inertial navigation system (INS) protected by a new high, anti-jam GPS null steering antenna system. In the terminal phase, JASSM is guided by an imaging infrared seeker and a general pattern match-autonomous target recognition system that provides aimpoint detection, tracking and strike. It also offers growth potential for different warheads and seekers, and for extended range.
The passive IR sensor on JASSM is a medium wavelength sensor using a 256 X 256 focal plane array with an IFOV of 12 deg. Sensor is turned on with approximately 8 seconds to go to impact with a sampling rate of 5 Hz. There are normally about 10-15 good IR pictures to put into the automatic target correlating algorithm once the sensor comes up and stablizes. Sensor is mounted below the waterline but on centerline axis of the vehicle (i.e. it looks out the IR window on the lower forward portion of the munition).
The AGM-158 ( used on B-52H, F-16C/D, F/A-18E/F, F-15E, F-117, B-1B, B-2, P-3C and S-3B) weapon is required to attack both fixed and relocatable targets at ranges beyond enemy air defenses and incorporates a high degree of stealth to improve its ability to penetrate enemy air defenses(more than 200 miles with a ER v. at 500 miles). After launch, it will be able to fly autonomously over a low-level, circuitous route to the area of a target, where an autonomous terminal guidance system will guide the missile in for a direct hit.
The key performance parameters for the system are Missile Mission Effectiveness, range, and carrier operability.
JASSM's midcourse guidance is provided by a Global Positioning System (GPS)-aided inertial navigation system (INS) protected by a new high, anti-jam GPS null steering antenna system. In the terminal phase, JASSM is guided by an imaging infrared seeker and a general pattern match-autonomous target recognition system that provides aimpoint detection, tracking and strike. It also offers growth potential for different warheads and seekers, and for extended range.
The passive IR sensor on JASSM is a medium wavelength sensor using a 256 X 256 focal plane array with an IFOV of 12 deg. Sensor is turned on with approximately 8 seconds to go to impact with a sampling rate of 5 Hz. There are normally about 10-15 good IR pictures to put into the automatic target correlating algorithm once the sensor comes up and stablizes. Sensor is mounted below the waterline but on centerline axis of the vehicle (i.e. it looks out the IR window on the lower forward portion of the munition).
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