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Lockheed AIM-80 Hawk Air to Air Missile
Type: | Short range aerial intercept missile |
Service Use: | (A, B) 2048-2060 RDF Space Navy, Navy, Air Force, Space Marines, and
Marines. (C, D) 2055-2060 RDF Space Navy, Navy, Air Force, Space Marines, and Marines. |
Length: | 62 cm |
Diameter: | 18 cm |
Wingspan: | 36 cm |
Weight: | 68 kg |
Warhead: | (A, C) Fragmentation (B, D) Plasma |
Weight/Yield: | (A, C) 8 kg (B, D) 12 kg |
Propulsion: | Hybrid rocket engine |
Guidance: | Combined IIR, UV/visual and active radar/home-on-jam. |
Max Speed: | Mach 9.3 |
Acceleration: | 9.6 G |
Range: | 20 km (atmosphere), 63.3 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