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rocket motors
The operation of rocket motors is often accompanied by the development of powerful secondary vortices in the combustion chamber [1-3], The superposition of the secondary vortices on the main flow leads to the formation of a cellular flow structure.
      
Monte Carlo simulation algorithms are given which are intended for the calculation of the spectral emissivity of jets of combustion products of solid-propellant rocket motors (SRM).
      
For technological reasons many high-performance solid rocket motors are made from segmented propellant grains with non-uniform port geometry.
      
This research demonstrated that hybrid rockets offer a safe, reliable upper stage option that is a versatile, cost-effective alternative to solid rocket motors.
      
Comprehension of wall-injection flow in a channel in the presence of different geometric discontinuities is necessary as part of the general investigations concerning combustion instabilities of solid propellant rocket motors.
      
This sutdy concerns the prediction of the stability of segmented solid propellant rocket motors.
      
We have attempted in this study to analyse the potential unstable development occurring in solid propellant rocket motors.
      
A multilayered thick cylindrical shell under internal pressure and thermal loads applicable to solid propellant rocket motors
      
This analytical procedure is useful in the preliminary design analysis of solid propellant rocket motors.
      
An important step in this evaluation was the identification of deposition patterns and the quantification of ecosystem loading rates of exhaust constituents from the solid rocket motors (SRMs) in the area of the launch pad.
      
Ultrasonic testing is widely used in detection of disbonds in multilayer structures such as solid fuel rocket motors, which consist of steel, rubber laminate, and solid fuel.
      
The mechanical properties of solid rocket propellants are very important for good functioning of rocket motors.
      
The development of nuclear rocket motors and the first thermionic systems "Topaz" in the world was a very important achievement in space nuclear technology.
      
Work on domestically produced nuclear rocket motors
      
The history and basic results of work on nuclear rocket motors (NRMs) in Russia are presented.
      
The history of the development of the first domestic high-temperature gas-cooled reactor - a unique experimental reactor for testing the core of reactors for nuclear-powered rocket motors - is briefly reviewed.
      
Asynchronous excitation of high-frequency combustion in liquid-fuel rocket motors is investigated under the action of periodic variation in the critical cross-sectional area of the nozzle.
      
Future studies in the area of mixed solid fuels for rocket motors are predicted.
      
Dynamic interaction of condensed particles in the combustion chamber of a solid rocket motors
      
A study is made of the effect of dynamic interactions on the evolution of the particle size distribution of aluminum oxide and aluminum agglomerates in the combustion chamber of solid rocket motors.
      
 

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