Studies on Starting Thrust Oscillations in Dual-Thrust Solid Propellant Rocket Motors

Autor: S. Deepthi, S. K. Kumaresh, M. Arun, D. Aravind Kumar, J. Darshan Kumar
Rok vydání: 2012
Předmět:
Zdroj: Lecture Notes in Mechanical Engineering ISBN: 9788132210061
DOI: 10.1007/978-81-322-1007-8_39
Popis: In this paper numerical studies have been carried out to examine the starting transient flow features of dual-thrust motors (DTMs) during the pre-ignition chamber conditions. Numerical computations have been carried out with the aid of a standard k-ω turbulence model. We concluded from the numerical results that in DTMs with highly loaded propellants the hot igniter gases can create pre-ignition thrust oscillations due to flow unsteadiness and recirculation. Under these conditions the convective flux to the surface of the propellant will be enhanced, which will create multiple-flame fronts leading to undesirable start-up transient. We also concluded that the prudent selection of the port geometry, without altering the propellant loading density, for damping the total temperature fluctuations within the motor is a meaningful objective for the suppression and control of instability and/or pressure/thrust oscillations often observed in solid propellant rockets with non-uniform port geometry.
Databáze: OpenAIRE