NASA NTRS · 19670055250
Preignition phenomena in small A-50/NTO pulsed rocket engines.
Abstract
Preignition phenomena in small Aerozine- 50/nitrogen tetroxide pulsed rocket engines shown partly due to hydrazine nitrate accumulation
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Christos, T., James, H. K., Miron, Y., Perlee, H. E.. 1967-07-01. Preignition phenomena in small A-50/NTO pulsed rocket engines.. https://ntrs.nasa.gov/citations/19670055250
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