A system analysis of the shuttle orbiter baseline system management (SM) computer function is performed. This analysis results in an alternative SM design which is also described. The alternative design exhibits several improvements over the baseline, some of which are increased crew usability, improved flexibility, and improved growth potential. The analysis consists of two parts: an application assessment and an implementation assessment. The former is concerned with the SM user needs and design functional aspects. The latter is concerned with design flexibility, reliability, growth potential, and technical risk. The system analysis is supported by several topical investigations. These include: treatment of false alarms, treatment of off-...
The approach used in the study, the operation of the various analytical procedures, and the developm...
Results are presented of systems analyses of the avionics software of the space shuttle orbiter
Space shuttle subsystem interface description, subsystem computational requirements, and analysis pr...
The findings are presented of investigations on concepts and techniques in automated performance ver...
An overview of the executive system design task is presented. The flight software executive system, ...
A study for the selection of a low cost shuttle system for design and development was conducted. The...
An analysis was conducted of the space shuttle propulsion systems to define the onboard checkout and...
Development of onboard checkout equipment and performance monitoring capability for space shuttles -...
Near term, cost effective concepts were defined to augment the power and duration capability offered...
Criteria and concepts for onboard checkout and monitoring system for space shuttle propulsion system...
The following tasks related to the FY 74 Shuttle Users Analysis were completed: (1) STS user charge ...
A baseline definition of the space shuttle mission simulator is presented. The subjects discussed ar...
Potential modes of operating in space in the space shuttle era are documented. The October 1973 NASA...
System concepts were characterized in order to define cost versus benefits for autonomous functional...
A methodology for developing balanced designs of spacecraft subsystems which interrelates cost, perf...
The approach used in the study, the operation of the various analytical procedures, and the developm...
Results are presented of systems analyses of the avionics software of the space shuttle orbiter
Space shuttle subsystem interface description, subsystem computational requirements, and analysis pr...
The findings are presented of investigations on concepts and techniques in automated performance ver...
An overview of the executive system design task is presented. The flight software executive system, ...
A study for the selection of a low cost shuttle system for design and development was conducted. The...
An analysis was conducted of the space shuttle propulsion systems to define the onboard checkout and...
Development of onboard checkout equipment and performance monitoring capability for space shuttles -...
Near term, cost effective concepts were defined to augment the power and duration capability offered...
Criteria and concepts for onboard checkout and monitoring system for space shuttle propulsion system...
The following tasks related to the FY 74 Shuttle Users Analysis were completed: (1) STS user charge ...
A baseline definition of the space shuttle mission simulator is presented. The subjects discussed ar...
Potential modes of operating in space in the space shuttle era are documented. The October 1973 NASA...
System concepts were characterized in order to define cost versus benefits for autonomous functional...
A methodology for developing balanced designs of spacecraft subsystems which interrelates cost, perf...
The approach used in the study, the operation of the various analytical procedures, and the developm...
Results are presented of systems analyses of the avionics software of the space shuttle orbiter
Space shuttle subsystem interface description, subsystem computational requirements, and analysis pr...