PERUN is the ideal choice for suborbital space flights. It is a single-stage guided suborbital launch vehicle powered by a hybrid rocket engine, designed to provide high performance at a low cost of operation.
payload mass
apogee
micro – G
50 kg
150 km
300 s
TECHNICAL OVERVIEW
height
diameter
lift – off weight
11.5 m
0.45 m
970 kg
ADVANTAGES
- Controlled flight path
- Trajectory accurate determination
- Low ascent accelerations
- Controlled re-entry orientation
- Simple preparations and transportation
- Simple pre-launch operations
- Late payload access
PERUN FLIGHT PROFILE
PROPULSION
SpaceForest is one of the pioneers globally utilizing green propellants for its hybrid rocket engines. Perun rocket uses the SF 1000 engine, the largest SpaceForest engine.
propellant
total impulse
thrust
burn time
modified paraffin
1.2 MNs
30 kN
50 s
PAYLOAD MODULES
SpaceForest offers three different payload modules (PM) to accommodate different payload volumes. The PM will be provided to the customer to mount their payload and send it back to SpaceForest for integration before a flight. Payloads can be sent directly to SF to handle the mounting and integration as well.
payload specs.
PM-1
PM-2
PM-3
height [mm]
200
350
450
diameter [mm]
377
377
377
weight [kg]
12.5
17.5
25
RECOVERY
The recovery system of PERUN is one of the main subsystems that guarantee the project’s successful operation. Following the reusability concept, the rocket is to be guided back using controlled parachutes to land within the predetermined landing zone.
COMMUNICATION
The autonomous tracking and data exchange system RASEL allows for reliable, long-distance communication with a rocket and continuous monitoring of the vehicle and payload parameters. The rocket position is continuously transmitted to the flight control center to ensure flight safety and quick recovery after landing. The communication system will also be used to download or upload data from the payload in real-time.
TRANSPORTER ERECTOR LAUNCHER
Focusing our engineering efforts on reducing the launch costs we developed the TEL – Transporter Erector Launcher to offer mobility and availability to launch from various spaceports around the world.
