Pyro Based Systems in Fin Locking Mechanism for Missile Applications

Abstract

A Pyro based mechanism is used in flight vehicles for control of fins. Here, a Pyro pin puller based lock and release mechanism has been designed to lock (arrest the movement of) the control fins when the missile is under carriage condition and to unlock when the missile clears the nose tip of aircraft after launch. This is a very critical mechanism as far as the launch of the missile is concerned. The dimensions of the individual components are derived from the classical design approach. The modelling of the components has been done by using solid works and the analysis is carried out using ANSYS.

Authors and Affiliations

D Smitha, Vinay Kiran Kolanu Biksha, R Venkateshwar

Keywords

Related Articles

OPTIMIZATION OF STACKING SEQUENCE OF COMPOSITE CYLINDRICAL SHELLS USING GENETIC ALGORITHM

Optimization of stacking sequence would enable the designer to efficiently exploit tailoring abilities of such filament wound cylinders. Hence, the main aim of the paper was to perform optimization of stacking sequence u...

The Generic Compact Automatic Test Equipment(GCATE) Based on Serial Communication for Fighter Aircrafts

Different Test Equipment (TE) required for the testing of serial communication based avionics systems for different aircrafts are usually supplied by the corresponding manufacturer. So procurement and maintenance of diff...

Performance Evaluation of Absorption Refrigeration Systems using Intelligent Optimization Techniques: A Review

Absorption refrigeration technologies have developed to provide enormous contribution to the industrial as well as residential applications. Providing cooling by utilization of renewable energy mediums as low grade heat...

A Critical Review on Traction Control System

This paper shares an investigation of vehicle footing control and examines its significance in interstate mechanization. A vigorous control technique is intended for slip control, which thus controls the footing. It is i...

Eliminating Wrong Spot Welding by Robots in Production Line

The main objective of our project is to reduce the false seam joints. There are many important issues, such as waiting for a lost robot, checking individual parts, unnecessary manual nutrition and increasing the cycle ti...

Download PDF file
  • EP ID EP672250
  • DOI 10.24247/ijmperdoct201963
  • Views 77
  • Downloads 0

How To Cite

D Smitha, Vinay Kiran Kolanu Biksha, R Venkateshwar (2019). Pyro Based Systems in Fin Locking Mechanism for Missile Applications. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD ), 9(5), 715-724. https://europub.co.uk/articles/-A-672250