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NASA NTRS ยท 20020068797

Advanced Computing Technologies for Rocket Engine Propulsion Systems: Object-Oriented Design with C++

Abstract

This document explores the use of advanced computer technologies with an emphasis on object-oriented design to be applied in the development of software for a rocket engine to improve vehicle safety and reliability. The primary focus is on phase one of this project, the smart start sequence module. The objectives are: 1) To use current sound software engineering practices, object-orientation; 2) To improve on software development time, maintenance, execution and management; 3) To provide an alternate design choice for control, implementation, and performance.

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BibTeXRIS

Gete Bekele. 2002-07-01. Advanced Computing Technologies for Rocket Engine Propulsion Systems: Object-Oriented Design with C++. https://ntrs.nasa.gov/citations/20020068797

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