Stability of combustion in solid-propellant rocket motors with pressure stabilization system
โ Scribed by S. A. Rashkovskii; Yu. M. Milekhin; A. V. Fedorychev; I. G. Assovskii
- Book ID
- 110160683
- Publisher
- SP MAIK Nauka/Interperiodica
- Year
- 2009
- Tongue
- English
- Weight
- 218 KB
- Volume
- 428
- Category
- Article
- ISSN
- 0012-5016
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๐ SIMILAR VOLUMES
The dynamical model of combustion in liquid propellant rocket motors is an unstable time-delay system. When it is stabilized by alinear state feedback controller, the robustness of the closed-loop system is not satisfactory. In this paper a variable structure control approach to stabilize the combus
## Abstract The reactions of stabilizers with the individual reactive species known to be generated during double base propellant decomposition, viz. NO~2~, HNO~2~ and HNO~3~, have been thoroughly investigated in an attempt to obtain information on the reactions that take place in these propellant