University of Hertfordshire

By the same authors

Design, Commissioning and Control System of a Hybrid Rocket Test Cell

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Documents

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Original languageEnglish
Title of host publicationProcs 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conf & Exhibit
PublisherAIAA
Volume2010
Publication statusPublished - 2010
Event46th AIAA/ASME/SAE/ASEE Joint Propulsion Conf & Exhibit - Nashville, United States
Duration: 25 Jul 201028 Jul 2010

Conference

Conference46th AIAA/ASME/SAE/ASEE Joint Propulsion Conf & Exhibit
Country/TerritoryUnited States
CityNashville
Period25/07/1028/07/10

Abstract

A rocket-motor test cell, capable of carrying out instrumented firings of hybrid and composite motors of up to 5kN (1100lb) thrust and up to 8 feet in length, has been installed at the University of Hertfordshire, UK. The key features and requirements of the design are described, especially with regard to the hazards considered. Details of the control system design are also discussed. The paper details the safety features, interlocks and operational safety considerations incorporated, then concludes with a discussion of the operational experience gained over more than sixty firings of all types, a review of the modifications made and how the design and implementation might have been improved in light of this experience.

Notes

Copyright © 2010 by University of Hertfordshire. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission.

ID: 447628