AIM-801 Sabre
From WikiStates
| AIM-801 Sabre | |
|---|---|
| Type | Medium Range Air to Air Missile |
| Place of origin | |
| Service history | |
| Used by | |
| Wars | None |
| Production history | |
| Designer | Scapa Aerospace Industries |
| Manufacturer | Scapa Aerospace Industries |
| Unit cost | $400,000 |
| Variants | AIM-801B |
| Specifications | |
| Weight | 175kg |
| Length | 3.75m (with booster) |
| Diameter | .17 m |
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| Warhead | Continuous Rod |
| Warhead weight | 18 kg |
| Detonation mechanism |
FZU-108 "Smart" anti-clutter proximity fuse and an impact crush fuse |
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| Engine | Ark Propulsion Mark-801 solid fuel rocket |
| Wingspan | 1.00m |
| Operational range |
200km |
| Flight ceiling | 25,000m |
| Speed | Mach 3.5 |
| Guidance system |
Cruise Phase Guidance: AN/DSN-1403 'Black Shift' Advanced Tactical Positioning System [Mid-course updates provided via data link] Terminal Guidance: AN/DPG-802 Phased Array Radar [Home-on-emissions capable] [900W] or AN/DAG-800 EO-IR [IR + 320×240 pixel dual waveband electro-optical imaging seeker, lock on after launch, 100 degree off bore sight acquisition, with infrared counter-counter-measures (IRCCM)] |
| Launch platform |
Aircraft |

