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2 search results for "propellant combustion rate"
20.1.2020 Studying the possibility of alternating delivery of rocket propellant wastes to a common thermal neutralization facility
The advantages of thermal neutralization units are considered, their operating principle is described, by the example of high-temperature toxic rocket propellants, the [...]
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10.1.2020 Calculation and selection of parameters for a propellant consumption diagram of dual-thrust main SRM
The equations obtained show that the required parameters of diagrams (including consumption-thrust characteristics difference between the starting and cruise modes) can be ensured [...]
Read more 10.1.2020 Calculation and selection of parameters for a propellant consumption diagram of dual-thrust main SRM