The Swift Striker (SS-1) is a Group 2 tactical loitering munition with a field-proven design that gives ground and naval forces an organic precision strike capability at the tactical edge. Launched from a vehicle or ground rail with no runway required for rapid deployment, it loiters for up to 1 hour and delivers a 5 kg multi-option warhead out to 100 km alongside modular payloads, with man-in-the-loop terminal guidance for precise effects and full abort authority to the final seconds of engagement.
EO/IR seeker with operator-directed terminal engagement. Abort and wave-off capability preserves positive control and minimizes collateral damage.
5 kg payload configurable with HE-fragmentation (standard) warheads to match the target set.
Vehicle or ground rail launch from unprepared sites. Single-vehicle transportable, deployed and operated by a two to three person crew.
1-hour endurance and 100 km reach let a single SS-1 find, fix, track, and finish targets deep beyond the forward line.
Day/night target acquisition and man-in-the-loop terminal guidance, with operator abort and wave-off authority through the final seconds of an engagement.
Feeds precise air data to the autopilot and carries the encrypted C2 and full-motion-video link, keeping the operator in control out to 100 km line of sight.
Houses the 5 kg multi-option warhead (HE-fragmentation standard) alongside the anti-jam GNSS/INS navigation suite.
A compact tandem-wing layout with endplate fins keeps span to just 1.5 m, giving stable low-speed loiter, a clean rail launch, and a footprint that fits on a single vehicle.
8-liter fuel load sustains 1 hour on station and a 100 km strike radius.
Single-cylinder 2-stroke gasoline engine in the ~50 cc class drives a rear-mounted pusher propeller for a 150 km/h cruise and a 210 km/h dash.
Technical Specification |
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|---|---|
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Air vehicle class |
Group 2 tactical loitering munition |
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Type |
Fixed-wing, pusher propeller, composite airframe |
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Length |
1.4 m (4.6 ft.) |
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Wingspan |
1.5 m (4.9 ft.) |
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Maximum take-off weight |
~ 18 kg (~ 40 lbs.) |
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Range |
100 km (54 NM) |
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Cruise speed |
150 km/h |
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Maximum speed |
210 km/h |
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Launch method |
Vehicle or ground rail launcher, runway independent |
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Power Plant |
Single-cylinder 2-stroke gasoline, pusher: ~50 cc class |
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Endurance |
1 hour |
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Recovery method |
Parachute recovery |
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Operational Radius (LOS datalink) |
80 to 100 km |
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Altitude Ceiling |
4,000 m (13,100 ft.) AMSL |
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Fuel Capacity |
8 L |
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Navigation |
GPS/GNSS autopilot with waypoint navigation, anti-jam options |
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Guidance |
EO/IR seeker, man-in-the-loop terminal, abort/wave-off |
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Payload capacity |
5 kg (11 lbs.) |
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Payload Options |
EO/IR seeker with laser rangefinder/designator; ISR package (EO/IR); encrypted C2/FMV datalink; anti-jam GNSS/INS. |
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Crew / footprint |
2 to 3 operators, single-vehicle transportable; ~ 30 min to launch |
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