NASA NTRS · 19680004293
All-fluid amplifier development for liquid rocket secondary injection thrust vector control Final report
Abstract
Staged vortex amplifier with integral gas generators for liquid rocket secondary injection thrust vector control
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Delozier, T. R., Kasselmann, J. T.. 1967-11-01. All-fluid amplifier development for liquid rocket secondary injection thrust vector control Final report. https://ntrs.nasa.gov/citations/19680004293
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