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General Dynamics AIM-90 Pegasus Air to Air Missile
| Type: | Short range aerial intercept missile |
| Service Use: | (A, B) 2061-2070 RDF Space Navy, Navy, Air Force, Marines, and Space Marines. |
| Length: | 65 cm |
| Diameter: | 18 cm |
| Wingspan: | 38 cm |
| Weight: | 73 kg |
| Warhead: | (A) Plasma (B) Fragmentation |
| Weight/Yield: | 14 kg |
| Propulsion: | Hybrid rocket engine |
| Guidance: |
(A, B) Combined IIR, UV/visual and active radar/home-on-jam with AI interface. |
| Max Speed: | Mach 10.3 |
| Acceleration: | 9.7 G |
| Range: | 26 km (atmosphere), 85.2 kps delta-v (space), |
| Platforms: |
History:
Layout adapted from Robotech
Reference Guide
Content by Jeffrey R. Spillner Page Last Updated on January 6, 2001 @ 11:00 GMT
Copyright © 1998-2001 Jeffrey R. Spillner