NASA NTRS · 19690039803
A basic study of ignition of hypergolic liquid propellants.
Abstract
Liquid hydrazine ignition by nitrogen tetroxide gas based on stagnation flow principle, presenting threshold measurements
Keep this discovery
Explore connections, maps & timelines
Breen, B. P., Kushida, R., Zung, L. B.. 1968-10-01. A basic study of ignition of hypergolic liquid propellants.. https://ntrs.nasa.gov/citations/19690039803
Cite the original work for its findings. Save a collection to share your selection of sources.