Abstract

Modifications achieved in the ignition delay time of shellac-based pyrotechnic igniter using different additives of varying particle size are observed and compared. 40 different pyrotechnic compositions were prepared using five additives i.e. aluminium, magnesium, red iron oxide, naphthalene and activated carbon. Four particle sizes i.e. <75 µm, 75-150 µm, 150-300 µm, 300-600 µm and two weight percentages of the additives i.e. 3% and 5% were investigated. A base composition, without any additive, was also prepared to compare and investigate the effects of additives and their particle size on the ignition delay time of the composition. The incorporation of additives significantly reduced the ignition delay time of the base composition. Addition of 5% red iron oxide having a particle size of <75 µm, delivered the maximum decrement in ignition delay time i.e. by 49.7%. Naphthalene of particle size of <75 µm added as 3% in the composition weight, provided the minimum reduction in the ignition delay time i.e. by 13.7%. It was also observed that all of the additives exhibited a similar manner of decrement in ignition delay time as the particle size decreased, except for naphthalene which exhibited an opposite trend.

Highlights

  • Composite Solid Propellant (CSP) rockets require an ignition device, called a pyrotechnic igniter, to initiate the burning process of the propellant grain

  • The energy input is converted into heat energy output which is transferred to the propellant surface (Kulkarni et al 1982; Sivan and Hass 2015)

  • The present study aims to investigate the effects and modifications achieved in the ignition delay time of shellac-based pyrotechnic igniter through the incorporation of different additives having different particle sizes

Read more

Summary

Introduction

Composite Solid Propellant (CSP) rockets require an ignition device, called a pyrotechnic igniter, to initiate the burning process of the propellant grain. Electrical, mechanical, chemical, shock-induced, laser or the combinations of these methods are used as the energy input sources to start the ignition process. An electric charge is used to start the ignition by providing the required heat energy for the chemical reaction to take place (Danali et al 2010). The ignition delay time is defined as the time interval between when the signal is received for initialization of the heat source and when the first bit of the grain burns.

Methods
Results
Conclusion
Full Text
Paper version not known

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call

Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.