NASA NTRS · 19930094405
Recent Results in Rocket Flight Technique
Abstract
The concept of the effective ejection velocity of a rocket engine is explained and the magnitude of the attainable ejection velocity theoretically and experimentally investigated. Velocities above 3000 meters per second (6700 mph) are actually measured and the possibilities of further increases shown.
Keep this discovery
Explore connections, maps & timelines
Sanger, Eugen. 1942-04-01. Recent Results in Rocket Flight Technique. https://ntrs.nasa.gov/citations/19930094405
Cite the original work for its findings. Save a collection to share your selection of sources.