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NASA NTRS · 19680040416

Ignition transients in small hypergolic rockets.

Abstract

Factors influencing rocket ignition pressures and conditions leading to large ignition overpressures, estimating residual propellant in rocket combustor

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BibTeXRIS

Juran, W., Stechman, R. C.. 1968-03-01. Ignition transients in small hypergolic rockets.. https://ntrs.nasa.gov/citations/19680040416

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