4 edition of Integrated controls and health monitoring for chemical transfer propulsion found in the catalog.
Integrated controls and health monitoring for chemical transfer propulsion
by NASA, For sale by the National Technical Information Service in [Washington, D.C.], [Springfield, Va
Written in English
|Statement||Marc G. Millis and Michael P. Binder ; prepared for the 26th Joint Propulsion Conference cosponsored by the AIAA, SAE, ASME, AND ASEE, Orlando, Florida, July 16-18, 1990.|
|Series||NASA technical memorandum -- 103185.|
|Contributions||Binder, Michael P., United States. National Aeronautics and Space Administration.|
|The Physical Object|
|Number of Pages||10|
tions for marine engine control and monitoring tailored for the vessel and its application. Based on the depth of knowl-edge within the company, these can range from standard systems to speciﬁ cation built systems to suit all applications. Propulsion Systems The Propulsion Control Panel is . The 6th edition of this book is a revision of the leading reference for rocket propulsion courses offered in aerospace engineering departments and in industry. It covers the basic physical principles of rocket propulsion such as nozzle thermodynamics, heat transfer, flight performance and fuel chemistry.
Factors affecting the implementation of Flight/Propulsion Control Integration (FPCI) techniques for energy management are considered. Elements of fly-by-wire control augmentation systems, electronic engine controls, advanced pilot displays, and automatically controlled inlet and nozzle systems in future aircraft designs are by: 4. Chemical and Electrical Propulsion Systems Space for Education, Education for Space •System or Control Mass (CM): –is a collection of matter of fixed identity –it may be considered enclosed by an invisible, massless, flexible surface through which no matter can pass –the boundary of the system may change position, size, and shape.
Propulsion Controls Engineering was established in San Diego, California on Aug by John P. (Jack) Reilly, Morley J. (Joe) Clapp, and Jim Humphreys, three former civilian employees of NAVSEACENPAC, who realized an increasing demand within the Navy for their technical expertise. ion propulsion system on DS1: 1. Adequate engine life—Prior to the NSTAR project, no ion engine intended for primary propulsion had ever been successfully operated for its full design life. 2. Guidance, navigation and control (GN&C) of a solar-electric propulsion (SEP) spacecraft—The low-thrust nature of SEP, together with large solar File Size: 2MB.
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Get this from a library. Integrated controls and health monitoring for chemical transfer propulsion. [Marc G Millis; Michael P Binder; United States.
National Aeronautics and Space Administration.]. 13 • Integration benefits flight and propulsion control • Enables optimum engine operating modes • More choices for alternate paths or components during flight with failed or marginal components • Enhances Vehicle Health Management • Can result in increased fuel efficiency, engine life • Advances Environmental Control for better cooling.
Marc G. Millis. BS Physics, MS Physics Entrepreneurship Integrated controls and health monitoring for chemical transfer propulsion. A candidate architecture for monitoring and.
the Propulsion System Health Management Element of the NASA Aviation Safety Program. The objective of this contract was to develop and demonstrate candidate engine health management technologies for enhanced aviation safety. The technologies included a General Electric Global Propulsion Health Monitoring for Enhanced Safety.
Integrated Flight / Propulsion Control Applications 3rd NASA GRC Propulsion Controls and Diagnostics Workshop February 28 – March 1, Cleveland, Ohio This document does not contain technical data within the definition contained in the International Traffic Arms Regulations (ITAR) and the Export Administration Regulations (EAR), as such is.
In the integrated flight propulsion control system, the integration control laws are developed as an off-line process and stored in an on-board computer for implementation. Also real-time optimization improves the performance further compared to pre-programmed optimization.
This results in an optimum integrated flight propulsion Size: 1MB. Controls and Health Management Technologies for Intelligent Aerospace Propulsion Systems NASA/TM— February National Aeronautics and Space Administration Glenn Research Center Prepared for the 42nd Aerospace Sciences Meeting and Exhibit sponsored by the American Institute of Aeronautics and Astronautics Reno, Nevada, January 5 File Size: 3MB.
The objective of the Intelligent Controls and Diagnostics for Propulsion Systems (ICDPS) research effort is to develop and validate advanced control system and health monitoring technologies that are critical to enhancing the safety, reliability and operability of aerospace propulsion systems.
The. American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA Hence, an integrated sensor system for control and condition monitoring of important components and parameters within the GTE is a primary requirement for the smooth operation of the GTE [9,10].
The ability to monitor the structural health of the rotating components, especially in the hot sections of turbine engines, is of major interest to aero community in improving engine safety and reliability.
The use of instrumentation for these applications remains very challenging. It requires sensors and techniques that are highly accurate, are able to operate in a high temperature Cited by: 7. Structural health monitoring involves the evaluation of a structure's capability to carry useful load. Structural health monitoring is being given greater emphasis as a result of the interest in extending the life of equipment and facilities as long as possible (Gerardi and.
Chemical rocket engines exist for a wide range of thrusts, from N up to 10 7 N. They are the only ones up to now that have been powerful enough to lift a spacecraft from the Earth’s surface (launcher—primary propulsion system).Author: Martin Tajmar.
The Chemical Propulsion Information Analysis Center (CPIAC) is one of several United States Department of Defense (DoD) sponsored Information Analysis Centers (IACs), administered by the Defense Technical Information Center (DTIC).
CPIAC is the oldest IAC, having been in continuous operation since when it was founded as the Rocket Propellant Information Agency as part of the Headquarters: Columbia, Maryland.
A candidate architecture for monitoring and control in chemical transfer propulsion systems. MICHAEL BINDER and; Prelaunch Expert System for Space Shuttle propulsion system health monitoring. JAMES ENGLE, DON BOGART and; JOHN MARINUZZI; Integrated air vehicle/propulsion technology for a multirole fighter- A MCAIR perspective.
Microwave Blade Tip Clearance/Blade Tip Timing Sensors. The ability to monitor the structural health of the rotating components, especially in the hot sections of turbine engines, is of major interest to aero community in improving engine safety and reliability .In addition, the active control and minimization of the gap between the rotating turbine blades and the stationary case of gas Cited by: 7.
Health Monitoring of Propulsion and Steering Devices Arthur Boogaard Eddy Engels Conference Houston, Texas Arthur Boogaard Eddy Engels Albert Wesselink Wärtsilä Propulsion The Netherlands.
2 Contents zIntroduction Wärtsilä Propulsion zSteerable Thrusters design philosophy Health monitoring Wärtsilä engines. power distribution among the devices based on the measured health will give an extension of its use. For propulsion and steering devices, actuated by hydraulic means, three aspects are of importance for health monitoring: 1.
Lubrication oil state, such as water ingress, seizes and amount of metal particles and state of. The book is intended to provide a one-stop resource for understanding the design of modern turbine engine control and monitoring systems. It can also be used as a reference for engineers and researchers designing control and monitoring systems for other industrial equipment and systems.
Jaw is a scientific monitoring consultant. Propulsion will play a significant role in determining whether the goals of SSTO will be achieved in the RLV program. Performance of the only high thrust reusable engine in the nation, the SSME, has been excellent, but the SSME does not have the sea-level F/W ratio needed to place an adequately sized SSTO vehicle into the required orbits.
propulsion system integrity during the System Development & Demonstration phase of a program and sustainment. These procedures describe the tasks necessary to attain knowledge that will allow systems engineering for the propulsion system to be accomplished in a cost-effective manner.
Size: KB.An Integrated Vehicle Propulsion and Power System for Long Duration Cryogenic Spaceflight Frank Zegler 1 United Launch Alliance, Centennial, CO, Abstract Proposed crewed exploration activities demand that high-performance, cryogenically fueled, in-space stages perform high delta-V missions that range from days to months in duration.
Although.PCMU - Propulsion Control and Monitor Unit. Looking for abbreviations of PCMU? It is Propulsion Control and Monitor Unit. Project Coordination and Monitoring Unit: PCMU: Pulse Code Modulation mu-law: PCMU: Pacific Marine Credit Union (Barstow, CA) Propulsion Aerodynamic Controls Integrated Research; Propulsion and Auxiliaries.