Peremoha
Product descripton: Peremoha by Volatus Aerospace
The Peremoha is a lightweight, hand-launched fixed-wing ISR UAS designed for long-endurance surveillance, reconnaissance, mapping, electronic warfare, and fire-control missions. Built around a common airframe and control system, it supports multiple mission configurations while maintaining a compact and easily deployable operational profile.
With up to 120 minutes of base endurance, a 30 km standard range, and a 7.4 kg normal take-off weight, Peremoha is optimized for persistent tactical observation and rapid mission adaptation. Its modular payload architecture allows the same aircraft to be configured for different sensing and mission requirements.
Key Operational Capabilities
- Hand-launched fixed-wing configuration
- Up to 120 minutes base endurance
- Up to 3 hours endurance in the extended EW configuration
- 30 km standard operational range, extendable to 40 km with mesh/tracking
- 100 km/h maximum speed
- Modular payload architecture using a common aircraft and control system
- Low acoustic signature, described as silent above 200 m AGL
- Payload options for daylight, thermal, low-light, mapping, and EW missions
- GPS-denied navigation capability based on terrain scanning
- Common handheld ground control system across mission configurations
Primary Mission Profiles
Tactical ISR & Surveillance
Long-endurance aerial observation using electro-optical and thermal imaging payloads for reconnaissance and target-location missions.
Fire Control
A dedicated sensor configuration combines low-light imaging, thermal imaging, and laser ranging for precision observation and ranging.
Electronic Warfare
An EW configuration supports additional mission equipment and extended endurance, with direction-finding and other specialized payload options.
Battlefield Mapping
Mapping configurations provide wide-area aerial imaging, including operation designed to maintain mapping capability in environments with datalink interference.
Technical specifications
| Parameter | Specification |
|---|---|
| Aircraft Type | Hand-launched fixed-wing ISR UAS |
| Wingspan | 2.4 m |
| Normal Take-Off Weight | 7.4 kg |
| Maximum Take-Off Weight | 11.5 kg |
| Maximum Speed | 100 km/h |
| Base Endurance | Up to 120 min |
| Extended EW Endurance | Up to 3 h |
| Standard Operational Range | 30 km |
| Extended Range | Up to 40 km with mesh/tracking |
| Power Source | Up to 4 × Li-Ion batteries |
| Payload Architecture | Modular / mission-specific |
| Navigation | GPS-denied terrain-scanning capability |
| Control System | Common handheld GCS |
| Acoustic Signature | Silent above 200 m AGL |
| Operating Temperature | −10°C to +40°C |