A New Test Rig for Measuring the Spin Stabilised Rocket Charcteristics

Authors

  • P.K. Roy Armament Research & Development Establishment, Pune
  • Vasantha Ramaswamy Armament Research & Development Establishment, Pune

DOI:

https://doi.org/10.14429/dsj.27.6697

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.

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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

Vol. 27 No. 4

Section

Short Communication

License

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