PERUN is the ideal choice for suborbital space flights. PERUN is a single stage guided suborbital launch vehicle powered by a hybrid rocket engine. Designed to provide high performance at a very low cost of operation.

 



 

Payload capacity

Vehicle Reusability

Turnaround time

50 kg

5 flights

6-8 hrs


 

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Download: brochure, user manual (IAC paper)

 


Technical Overview

 

Height

Diameter

Lift-off weight

10 m

0.5 m

950 kg

 


Advantages

  • Controlled flight path & Trajectory profile determination

  • Controlled ascent & descent accelerations

  • Controlled re-entry orientation

  • Fast payload integration

 


PERUN standard flight profile


Propulsion

SpaceForest is one of the pioneers globally utilizing green propellants for its hybrid rocket engines.

  • GREEN PROPELANTS
    BURN TIME
    40 s
    ACCELERATION
    < 6g
    MICROGRAVITY TIME
    4+ mins

 

 


Payload modules

SpaceForest offers three different payload modules (PM) to accomade different payload volumes. The PM will be provided to the customer to mount their payload and send it back to SpaceForest for integration before flight. Payloads can be sent directly to SF to handle the mounting and integration as well.

Allowable payload specs. PM-1 PM-2 PM-3
Height (mm) 200 350 450
Diameter (mm) 400 400 400
Weight (kg) 12.5 17.5 25
Maintenance access door 2 2 3
Payload access to space No No Yes
Payload ejection to space No No Yes

 

 

 


Recovery

The recovery system of PERUN is one of the main subsystems that guarantee the successful operation of the mission. Following the reusability concept, the rocket is to be guided back using controlled parachutes to land within the predetermined landing zone. Payloads can be accessed right after recovery operation is done thanks to the usage of safe system of depressurizing the rocket completely before touchdown.


Launch sites

SF is working on preparing launch sites for PERUN in cooperation with the Polish Space Aency POLSA, Swedish Space Corporation SSC and Andoya Space Center.

With focusing our engineering efforts to reduce the launch costs we developed the Transporter Erector Launcher TEL to offer mobility and availability to launch from various space ports around the world.

 

 

 

 

 


 

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