NASA NTRS · 19680064758
Application of trioxygen difluoride in liquid- rocket-propellant technology.
Abstract
Trioxygen difluoride additive rendering LOX hypergolic, discussing environmental limits of reliable hypergolic ignition with liquid and gaseous hydrogen
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Amster, A. B., Capener, E. L., Dickinson, L. A.. 1968-11-01. Application of trioxygen difluoride in liquid- rocket-propellant technology.. https://ntrs.nasa.gov/citations/19680064758
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