Video: VISERION hybrid rocket engine on the test bench
During the test runs at the facility at DLR's Trauen site, the catalytically decomposed hydrogen peroxide entered the combustion chamber at approximately 650 degrees Celsius. The heat released was converted into kinetic energy – providing approximately 12,000 newtons of thrust.
Video: VISERION hybrid rocket engine on the test bench
Video: VISERION hybrid rocket engine on the test bench
During the test runs at the facility at DLR's Trauen site, the catalytically decomposed hydrogen peroxide entered the combustion chamber at approximately 650 degrees Celsius. The heat released was converted into kinetic energy – providing approximately 12,000 newtons of thrust.
Credit: © DLR. All rights reserved
Duration:00:00:56