On Saturday, February 4th we tested our BPM-5 rocket engine. As something new, we used our pressurization system actively by changing the engine chamber pressure along the way. We tried to keep the O/F ratio Read more…
Fuel and LOX ratio BPM5 Rocket Engine Tests
On October 10th 2016 we put our BPM5 engine through the longest burn to date. In 35 seconds it provided a total impulse of 180.000 Ns. On the data overlay pressures are given in bar, Read more…
Testing the gimbal for the BPM-5 rocket engine. This was done on the 30th of october 2016
Copenhagen Suborbitals was featured in German TV: Galileo. www.galileo.tv
Animation of the July 23rd 2016 flight of Nexø I.
Nexø 1 Launch – Teaser
Final adjustmens of the ballute and parachute before launch of the Nexø 1 rocket.
Final adjustmens of the guidance system before launch of the Nexø 1 Rocket.
The 25th of June the NEXØ 1 rocket went through a SAT (Sea Acceptance Test). The purpose of this type of testing is to simulate a launch, down to the smallest detail and get through Read more…
