SPACEFOREST SPÓŁKA Z OGRANICZONĄ ODPOWIEDZIALNOŚCIĄ
- ul. Bolesława Krzywoustego 1 B, 81-035 Gdynia, Poland
- 5832860098
- marcin.sarnowski@spaceforest.pl
- www.spaceforest.pl
Description
A key area of SpaceForest’s activity is radar technology. The company designs and develops radar systems and subsystems, including RF front ends, antennas, transmitters, receivers, power amplifiers and dedicated software for real-time detection, tracking and situational awareness. Its flagship radar product, HUSSAR, is designed to support effective object detection and monitoring in challenging conditions, providing users with improved awareness, faster decision-making and greater operational security.
SpaceForest’s solutions are developed with a strong focus on customer value. The company supports partners who require robust, adaptable and high-performance technologies for applications such as border surveillance, critical infrastructure protection, unmanned platforms, perimeter security, defence operations and space-related missions. Thanks to in-house engineering capabilities, rapid prototyping and testing, SpaceForest can tailor its systems to specific technical and operational requirements.
In addition to radar systems, SpaceForest is active in rocket technologies and suborbital platforms, strengthening its position as an innovative technology partner for advanced aerospace and dual-use projects. Its experience in complex engineering programmes enables the company to reduce technological risk, accelerate development cycles and provide solutions ready for practical deployment.
By combining radar expertise, space engineering and flexible product development, SpaceForest helps customers enhance situational awareness, improve mission effectiveness and access modern technologies designed for the needs of civil, security and defence markets.
Products
Rocket length: approx. 11–12 m
Body diameter: approx. 0.45 m
Lift-off mass: around 900–1,000 kg, depending on mission setup
Payload capacity: up to 50 kg for experimental payloads and on-board systems
Propulsion: hybrid rocket engine using liquid oxidizer and solid fuel
Thrust class: approx. 40–50 kN
Total impulse: in the high suborbital-class range, mission- and engine-configuration dependent
Flight profile: vertical or near-vertical suborbital trajectory, designed to reach high-altitude test conditions, with a target apogee of up to approx. 150 km
Velocity: supersonic flight regime, depending on payload mass and trajectory
Recovery: reusable architecture with parachute-based recovery of the rocket section and payload module
System elements: PERUN rocket, mobile launch platform, and RASEL ground-support system for launch preparation, monitoring, telemetry, and mission control.