A rigorous propulsion system modelling method suitable for control and condition monitoring purposes is developed. Previously developed control oriented methods yielding nominal models for gaseous medium propulsion systems are extended to include both nominal and anomalous models for liquid mediums in the following two ways. First, thermodynamic and fluid dynamic properties for liquids such as liquid hydrogen are incorporated into the governing equations. Second, anomalous conditions are captured in ways compatible with existing system theoretic design tools so that anomalous models can be constructed. Control and condition monitoring based methods are seen as an improvement over some existing modelling methods because such methods typicall...
Rocket engine oscillating data can reveal many physical phenomena ranging from unsteady flow and aco...
A Hybrid Combustion Facility (HCF) was recently built at NASA Ames Research Center to study the comb...
Research on propulsion stability (chugging and acoustic modes), and propellant valve control was inv...
The work reported herein represents a continuation of work begun at MSFC during the 1991 NASA/ASEE S...
The objective of Phase I of this research effort was to develop an advanced mathematical-empirical m...
Dynamic models for liquid rocket engines are developed. The particular case of the Space Shuttle Mai...
As NASA continues to develop various advanced propulsion technologies for space exploration, two fac...
A prototype software system was constructed to detect anomalous Space Shuttle Main Engine (SSME) beh...
A diagnostic software package is currently being developed at NASA LeRC that utilizes qualitative mo...
Current research in intelligent control systems at the Lewis Research Center is described in the con...
The fluid flow-induced vibration of the Space Shuttle main engine (SSME) components are being studie...
A simplified model is presented of the space shuttle main engine (SSME) dynamics valid within the ra...
Approximately 85,000 liquid rocket engine failure reports, obtained from 30 years of developing and ...
Over the past several years, there has been an increased awareness in the necessity for rocket engin...
A chemical analysis of the emission and absorption spectra in the combustion chamber of a nitrogen t...
Rocket engine oscillating data can reveal many physical phenomena ranging from unsteady flow and aco...
A Hybrid Combustion Facility (HCF) was recently built at NASA Ames Research Center to study the comb...
Research on propulsion stability (chugging and acoustic modes), and propellant valve control was inv...
The work reported herein represents a continuation of work begun at MSFC during the 1991 NASA/ASEE S...
The objective of Phase I of this research effort was to develop an advanced mathematical-empirical m...
Dynamic models for liquid rocket engines are developed. The particular case of the Space Shuttle Mai...
As NASA continues to develop various advanced propulsion technologies for space exploration, two fac...
A prototype software system was constructed to detect anomalous Space Shuttle Main Engine (SSME) beh...
A diagnostic software package is currently being developed at NASA LeRC that utilizes qualitative mo...
Current research in intelligent control systems at the Lewis Research Center is described in the con...
The fluid flow-induced vibration of the Space Shuttle main engine (SSME) components are being studie...
A simplified model is presented of the space shuttle main engine (SSME) dynamics valid within the ra...
Approximately 85,000 liquid rocket engine failure reports, obtained from 30 years of developing and ...
Over the past several years, there has been an increased awareness in the necessity for rocket engin...
A chemical analysis of the emission and absorption spectra in the combustion chamber of a nitrogen t...
Rocket engine oscillating data can reveal many physical phenomena ranging from unsteady flow and aco...
A Hybrid Combustion Facility (HCF) was recently built at NASA Ames Research Center to study the comb...
Research on propulsion stability (chugging and acoustic modes), and propellant valve control was inv...