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Lockheed AGM-41 Nodachi Air to Ground Missile
Type: | Short range air to ground missile |
Service Use: | 2057-2070 RDF RDF Space Navy, Navy, Air Force, Space Marines, and Marines and SSS. |
Length: | 114 cm |
Diameter: | 26 cm |
Wingspan: | 34 cm |
Weight: | (A, D) 164 kg (B) 165 kg (C) 168 kg |
Warhead: | (A) Plasma (B) Napalm (C) Fragmentation (D) High Explosive Armor Piercing |
Weight/Yield: | (A, D) 20 kg (B) 16 kg (C) 24 kg |
Propulsion: | Hybrid rocket engine |
Guidance: | Combined IIR and active radar/home-on-jam with AI interface. |
Max Speed: | Mach 7.7 |
Acceleration: | (A, B, D) 6.1 G (C) 6.0 G |
Range: | 35 km (atmosphere), 52.6 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