The ST-10 is a Group 3 long-range loitering munition built to hold targets at risk deep inside contested territory. Launched from a vehicle or ground rail with no runway required, it flies out to 1,000 km under beyond-line-of-sight SATCOM control, loiters for up to 5 hours, and delivers a 10 kg multi-option warhead with man-in-the-loop precision, backed by anti-jam GPS/INS navigation for contested environments.
1,000 km range with beyond-line-of-sight SATCOM/relay command and control puts strategic targets within reach of tactical units.
10 kg payload configurable with HE-fragmentation, shaped-charge (anti-armor/anti-materiel), penetrator, or thermobaric warheads.
Anti-jam GPS/INS with backup navigation sustains the mission through GNSS-denied and electronically contested environments.
Vehicle or ground rail launch from dispersed, unprepared sites. Vehicle-transportable with a crew of two to three operators.
High-fidelity airspeed and attitude data keeps the autopilot precise across long-duration, 1,000 km mission profiles.
Stabilized day/night imaging with laser designation and man-in-the-loop terminal guidance, including operator abort and wave-off.
SATCOM/relay command link maintains positive control and full-motion video far beyond line of sight, across the full 1,000 km engagement envelope.
2.9 m high-aspect wing with winglets, tuned for a 5-hour loiter and precise terminal maneuvering.
Carries the 10 kg multi-option warhead (HE-fragmentation, shaped-charge, penetrator, or thermobaric) and a 40-liter fuel load for 1,000 km of reach.
Piston engine in the ~70 cc class, pusher configuration, delivering a 170 km/h cruise and a 200 km/h dash.
Technical Specification |
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|---|---|
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Air vehicle class |
Group 3 long-range loitering munition |
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Type |
Fixed-wing, pusher propeller, composite airframe |
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Length |
2.9 m (9.5 ft.) |
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Wingspan |
2.9 m (9.5 ft.) |
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Maximum take-off weight |
70 kg (154 lbs.) |
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Range |
1,000 km (540 NM) |
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Cruise speed |
170 km/h |
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Maximum speed |
200 km/h |
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Launch method |
Vehicle or ground rail launcher, runway independent |
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Power Plant |
Piston engine, pusher: ~70 cc class |
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Endurance |
5 hours |
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Recovery method |
Expendable munition |
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Operational Radius (LOS datalink) |
1,000 km |
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Altitude Ceiling |
5,000 m (16,400 ft.) AMSL |
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Fuel Capacity |
40 L |
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Navigation |
Anti-jam GPS/INS with waypoint navigation, BLOS command link |
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Guidance |
EO/IR seeker, man-in-the-loop terminal, abort/wave-off |
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Payload capacity |
10 kg (22 lbs.) |
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Payload Options |
EO/IR seeker; laser designator; BLOS SATCOM/relay C2; anti-jam GNSS/INS with backup navigation. Warhead options: HE-fragmentation, shaped-charge (anti-armor/anti-materiel), penetrator, thermobaric |
|
Crew / footprint |
2 to 3 operators with BLOS terminal, vehicle-transportable |
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