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Raytheon AGM-40 Murasame Air to Ground Missile
Type: | Long range air to ground missile. |
Service Use: | 2056-2070 RDF RDF Space Navy, Navy, Air Force, Space Marines, Marines and SSS. |
Length: | 600 cm |
Diameter: | 68 cm |
Wingspan: | 136 cm |
Weight: | (A, B) 860 kg |
Warhead: | (A) W-283 thermonuclear reaction warhead (B) High Explosive Armor Piercing |
Weight/Yield: | (A) Selectable from 50 kT to 300 kT (B) 230 kg |
Propulsion: | Hybrid rocket engine. |
Guidance: | (A) Combined IIR, inertial navigation system, active radar homing,
and Galactic Positioning System (GPS) with Permissive Action Link (PAL). (B) Combined IIR, inertial navigation system and active radar homing with Galactic Positioning System (GPS). |
Max Speed: | Mach 6.0 |
Acceleration: | 3.0 G |
Range: | 400 km (atmosphere), 156.1 kps delta-v (space) |
Platforms: |
History:
Layout adapted from Robotech Reference Guide
Content by Jeffrey R. Spillner
Copyright © 1998-2002 Jeffrey R. Spillner
Page Last Updated on January 21, 2002 @ 11:00 GMT