Second flight of Perun rocket
The second test flight of the Perun rocket took place at the Air Force Training Centre in Ustka. Its main purpose was primarily to test control algorithms, recovery, launch procedures and many other aspects that…
First flight of Perun rocket from Ustka
On June 21st Perun rocket was launched from the Air Force Training Centre in Ustka and reached an altitude of 22 km. During the flight, we tested the operation of several systems such as thrust…
Third place in the “Innovations for Security and Defense” competition
Our project was awarded in the “Innovations for Security and Defense” competition!Third place (ex aequo) in the competition organized under the honorary patronage of the Head of the National Security Bureau and the Director of…
New project: Reusable Strategic Space Launcher Technologies & Operations
SpaceForest sp. z o. o., an SME from Poland, is involved in SALTO (Reusable Strategic Space Launcher Technologies & Operations) project that will advance forward Europe’s first reusable rocket. Funded by the European Commission under…
Perun rocket prelaunch procedures tested at the Training Centre in Ustka
After reconnaissance at the Air Force Training Centre in Ustka last December, the time has come to practice prelaunch procedures of the Perun rocket. Last week, SpaceForest’s launch crew went to test the preparation of…
Perun ballute decelerator successful test
A ballute is a supersonic decelerator, designed for high velocity flow as an alternative to parachutes. Our version was developed to support the re-entry and recovery of PERUN rocket. After months of design and development,…
Second Thrust Vector Control successful test
Last week we tested the performance of the Thrust Vector Control (TVC) system, improved after the first flight conducted in August this year. The task of the 10-degree deflected BIGOS 6 rocket was to align…
Thrust Vector Control successful test
Thrust Vector Control – TVC, is one of two control systems of the PERUN rocket. TVC system allows to control the direction of the thrust vector of the main hybrid rocket engine, what enables control…
Successful final presentation of SF 1000 engine
During the presentation of the flight version of the SF 1000 engine, which took place on April 1st, 2022, it worked for over 43 seconds! The total impulse of the engine was 1.15 [MNs], which…
Rocket Engine SF 1000 Test
On January 28th, 2021, at the military training ground in Strzepcz, we achieved a milestone in the SIR project (Suborbital Inexpensive Rocket). Total impulse: 1260 kNsSpecific impulse: 211.9 s The controllable and recoverable suborbital rocket PERUN with…