ePrints@IIScePrints@IISc Home | About | Browse | Latest Additions | Advanced Search | Contact | Help

Ignition delay and unsteady temperature effects on ignition peak of solid rockets

Sanal Kumar, VR and Unnikrishnan, C and Raghunandan, BN (2002) Ignition delay and unsteady temperature effects on ignition peak of solid rockets. In: 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2002, 7-10 July 2002, Indianapolis, IN; United States.

[img]
Preview
PDF
AIAA_ASME_SAE_ASEE_JOI_PRO_CON_EXH_2002.pdf - Published Version

Download (143kB) | Preview
Official URL: https://dx.doi.org/10.2514/6.2002-3754

Abstract

The coupled and the uncoupled effects of the ignition delay and the unsteady combustion gas temperature on ignition peak of high velocity transient motors are examined with the help of a two dimensional Navier-Stokes solver. It has been observed through the parametric studies that the altered variation of the ignition delay will alter the transient temperature growth history and the flame spread mechanism, which in turn alter the pressure spike of identical solid rockets. It has been inferred that the altered variation of both the chamber pressure-rise rate and the ignition temperature will alter the ignition delay and thereby the overall starting transient history of solid rockets. It has been concluded that the solid rocket motor designers should have a bearing on the pressure and pressurization rate prior to ignition for achieving repeatability of starting transient history in solid motors with the same propellant formulation and geometry. © 2002 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.

Item Type: Conference Paper
Publication: 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Publisher: American Institute of Aeronautics and Astronautics Inc.
Additional Information: cited By 3; Conference of 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2002 ; Conference Date: 7 July 2002 Through 10 July 2002; Conference Code:103017
Keywords: Flame research; Navier Stokes equations; Pressurization; Propulsion; Rockets; Temperature, Ignition temperatures; Navier-Stokes solver; Pressurization rates; Solid rocket motors; Starting transient; Transient temperature; Unsteady combustion; Unsteady temperatures, Starting
Department/Centre: Division of Mechanical Sciences > Aerospace Engineering(Formerly Aeronautical Engineering)
Date Deposited: 28 Oct 2020 11:40
Last Modified: 28 Oct 2020 11:40
URI: http://eprints.iisc.ac.in/id/eprint/65839

Actions (login required)

View Item View Item