NASA NTRS · 19700036149
Hydrazine monopropellant provides 0.5-600 lb thrust
Abstract
Hydrazine monopropellant performance and characteristics, describing various catalysts and propulsion systems
Keep this discovery
Explore connections, maps & timelines
Price, T. W.. 1969-10-01. Hydrazine monopropellant provides 0.5-600 lb thrust. https://ntrs.nasa.gov/citations/19700036149
Cite the original work for its findings. Save a collection to share your selection of sources.