Add to ORKGThe tasks are defined required to design, develop produce, and field support a shuttle mission simulator for training crew members and ground support personnel. The requirements for program management, control, systems engineering, design and development are discussed along with the design and construction standards, software design, control and display, communication and tracking, and systems integration
The configuration and simulation studies of a C-8A (De Havilland Buffalo) aircraft are described. Th...
Systems and methods for providing dynamic control to a surface immersed in a dynamic fluid. The syst...
In Jan. 1991, the LaRc SSFO performed an assessment of the configuration characteristics of the prop...
The training requirements of all mission phases for crews and ground support personnel are presented...
The detailed shuttle mission simulator hardware requirements are discussed. The conceptual design me...
The guidelines for EVA and IVA tasks to be performed on the space shuttle are defined. In deriving t...
Asymptotic formulas for the characteristic root errors as well as transfer function gain and phase e...
The Space Station structure has been baselined to be a 5 M (16.4 ft) erectable truss. This structure...
Drawings are presented for equipment designed and fabricated to affect the integration of controller...
The g cueing system software design and implementation in the dual microprocessor system of the F-15...
The interface between tasks and the sequence of information flow are charted. The mission model and ...
The Manufacturing Progress Function is a mathematical technique which has been used in many industri...
Formal NASA technical reports, papers published in technical journals, and presentations by MSFC per...
Two important aspects of concurrent processing under development at TRW are discussed. These are: (1...
The following subject areas are covered: background (space propulsion facility assessment team final...
The configuration and simulation studies of a C-8A (De Havilland Buffalo) aircraft are described. Th...
Systems and methods for providing dynamic control to a surface immersed in a dynamic fluid. The syst...
In Jan. 1991, the LaRc SSFO performed an assessment of the configuration characteristics of the prop...
The training requirements of all mission phases for crews and ground support personnel are presented...
The detailed shuttle mission simulator hardware requirements are discussed. The conceptual design me...
The guidelines for EVA and IVA tasks to be performed on the space shuttle are defined. In deriving t...
Asymptotic formulas for the characteristic root errors as well as transfer function gain and phase e...
The Space Station structure has been baselined to be a 5 M (16.4 ft) erectable truss. This structure...
Drawings are presented for equipment designed and fabricated to affect the integration of controller...
The g cueing system software design and implementation in the dual microprocessor system of the F-15...
The interface between tasks and the sequence of information flow are charted. The mission model and ...
The Manufacturing Progress Function is a mathematical technique which has been used in many industri...
Formal NASA technical reports, papers published in technical journals, and presentations by MSFC per...
Two important aspects of concurrent processing under development at TRW are discussed. These are: (1...
The following subject areas are covered: background (space propulsion facility assessment team final...
The configuration and simulation studies of a C-8A (De Havilland Buffalo) aircraft are described. Th...
Systems and methods for providing dynamic control to a surface immersed in a dynamic fluid. The syst...
In Jan. 1991, the LaRc SSFO performed an assessment of the configuration characteristics of the prop...