Date of Award

2012-01-01

Degree Name

Master of Science

Department

Mechanical Engineering

Advisor(s)

Ahsan R. Choudhuri

Abstract

A liquid propulsion research facility has been developed at the Center for Space Exploration Technology Research at The University of Texas at El Paso. This facility has capabilities for producing up to 25 liters of Liquid Methane, feeding LOX/Methane propellants to 100 N class thrusters and conducting automated steady state and pulsing combustion experiments. This work describes the design, development and testing process of the Data Acquisition and Remote Control System developed to integrate an Altitude Simulation System, a Cryogenic Delivery System, and multiple rocket combustors and thrusters. A Torch Ignition System development is detailed as well as the evaluation process to characterize optimum operation when integrated to a Multi-purpose Combustor Test Rig.

Language

en

Provenance

Received from ProQuest

File Size

85 pages

File Format

application/pdf

Rights Holder

Jesus Betancourt-Roque

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