Transferring jet engine diagnostic and control technology to liquid propellant rocket engines
This paper presents the methodology for developing a diagnostic and control system for a current, operational jet engine. A description is given of each development stage, the system components and the technologies which could be transferred to liquid propellant rocket engines. Finally, the operational impact is described in terms of cost and maintenance based on actual jet engine experience. Efforts are continuing to develop new diagnostic techniques under IR D for application on the advanced technical fighter. Already improved techniques and application methods are becoming available. This technology is being evaluated and may also be transferred to rocket engine diagnostic and control system development.
- OSTI ID:
- 5523401
- Report Number(s):
- AIAA-Paper-89-2851; CONF-8907118-
- Resource Relation:
- Conference: 25. American Society of Mechanical Engineers joint propulsion conference, Monterey, CA (USA), 10-13 Jul 1989
- Country of Publication:
- United States
- Language:
- English
Similar Records
Current Status of the Nuclear-Powered Arc Jet Rocket Engine
Rocket Engine Test System for Development of Novel Propulsion Technologies