Model for nonlinear transient burning of hydrazinium nitroformate
other
Transient burning of solid propellants is a topic that still contains a large number of questions. The transient burning of neat hydrazinium nitroformate is calculated within the quasi-steady gas-phase, homogeneous one-dimensional condensed phase approach. We focus on the effect of the condensed phase on the transient burning of solid propellants by showing the effect of temperature-dependent thermal properties, phase transitions, and chemical reactions in the solid phase. By solving the governing equations numerically, the nonlinear effects are conserved.
TNO Identifier
131474
Source
Journal of Propulsion and Power, 15(6), pp. 778-782.
Publisher
TNO
Place of publication
Rijswijk
Pages
778-782
Files
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