A New Test Rig for Measuring the Spin Stabilised Rocket Charcteristics
Keywords:
Measuring chamber pressure, Forward thrust, Spin rate, Simulated flight conditions
Abstract
This article describes the general arrangement and function of a new test rig designed and fabricated by the authors for testing and measuring chamber pressure, forward thrust and spin rate developed by spin stabilised rockets on firing under simulated flight conditions.
Published
2014-10-01
How to Cite
Roy, P., & Ramaswamy, V. (2014). A New Test Rig for Measuring the Spin Stabilised Rocket Charcteristics. Defence Science Journal, 27(4), 155-156. https://doi.org/10.14429/dsj.27.6697
Issue
Section
Short Communication
Copyright (c) 2016 Defence Science Journal
Where otherwise noted, the Articles on this site are licensed under Creative Commons License: CC Attribution-Noncommercial-No Derivative Works 2.5 India