This paper describes the quantitative application of the theory of System Health Management and its operational subset, Fault Management, to the selection of Abort Triggers for a human-rated launch vehicle, the United States' National Aeronautics and Space Administration's (NASA) Space Launch System (SLS). The results demonstrate the efficacy of the theory to assess the effectiveness of candidate failure detection and response mechanisms to protect humans from time-critical and severe hazards. The quantitative method was successfully used on the SLS to aid selection of its suite of Abort Triggers
New commercial crew vehicles require an emergency detection system for crew abort capability. This s...
In order to support manned spaceflight safety requirements, the Space Launch System (SLS) has define...
The implementation of a new dispersion methodology is described, which dis-perses abort initiation a...
This paper describes the quantitative application of the theory of System Health Management and its ...
SHM/FM theory has been successfully applied to the selection of the baseline set Abort Triggers for ...
This paper describes a quantitative methodology for bounding the false positive (FP) and false negat...
Create an improved method to calculate reliability of a conceptual launch vehicle system prior to fa...
Lessons learned from past failures of launch vehicle developments and operations were used to create...
A method has been developed with the objective of making the potentially intractable problem of laun...
The engineering development of the new Space Launch System (SLS) launch vehicle requires cross disci...
Lessons learned from past failures of launch vehicle developments and operations were used to create...
For human spaceflight missions, a launch vehicle failure poses the challenge of returning the crew s...
In order to support manned spaceflight safety requirements, the Space Launch System (SLS) has define...
NASA is investigating the use of advanced automation to enhance crew productivity for Space Station ...
This paper covers the simulation and evaluation of a controller design for the Crew Module (CM) Laun...
New commercial crew vehicles require an emergency detection system for crew abort capability. This s...
In order to support manned spaceflight safety requirements, the Space Launch System (SLS) has define...
The implementation of a new dispersion methodology is described, which dis-perses abort initiation a...
This paper describes the quantitative application of the theory of System Health Management and its ...
SHM/FM theory has been successfully applied to the selection of the baseline set Abort Triggers for ...
This paper describes a quantitative methodology for bounding the false positive (FP) and false negat...
Create an improved method to calculate reliability of a conceptual launch vehicle system prior to fa...
Lessons learned from past failures of launch vehicle developments and operations were used to create...
A method has been developed with the objective of making the potentially intractable problem of laun...
The engineering development of the new Space Launch System (SLS) launch vehicle requires cross disci...
Lessons learned from past failures of launch vehicle developments and operations were used to create...
For human spaceflight missions, a launch vehicle failure poses the challenge of returning the crew s...
In order to support manned spaceflight safety requirements, the Space Launch System (SLS) has define...
NASA is investigating the use of advanced automation to enhance crew productivity for Space Station ...
This paper covers the simulation and evaluation of a controller design for the Crew Module (CM) Laun...
New commercial crew vehicles require an emergency detection system for crew abort capability. This s...
In order to support manned spaceflight safety requirements, the Space Launch System (SLS) has define...
The implementation of a new dispersion methodology is described, which dis-perses abort initiation a...