Add to ORKGThe detailed shuttle mission simulator hardware requirements are discussed. The conceptual design methods, or existing technology, whereby those requirements will be fulfilled are described. Information of a general nature on the total design problem plus specific details on how these requirements are to be satisfied are reported. The configuration of the simulator is described and the capabilities for various types of training are identified
The feasibility of shuttle orbiter docking to the Space Operations Center (SOC) is studied. The in-o...
Extensively axisymmetric and non-axisymmetric Single Stage To Orbit (SSTO) vehicles are considered. ...
Late in 1990, the NASA Systems Integration Group began functioning and the aircraft systems studies ...
The training requirements of all mission phases for crews and ground support personnel are presented...
The tasks are defined required to design, develop produce, and field support a shuttle mission simul...
Pilot/vehicle analysis techniques for optimizing aircraft handling qualities are presented. The anal...
The work under this grant has been directed to two aspects of the control of flexible spacecraft: (1...
Conceptual design studies were performed directed toward a high power, ultralightweight solar array,...
The Space Station structure has been baselined to be a 5 M (16.4 ft) erectable truss. This structure...
Software conceptual designs (SCD) are presented for meeting the simulator requirements for the shutt...
An outline of the organization and capabilities of the Engine Structures Computational Simulator (Si...
This report discusses the application and cost of two types of altimeter systems (spaceborne (satell...
An experimental flight test program was designed for the Total In Flight Simulator (TIFS) directed t...
Possible storable propellant configurations and program plans are evaluated for the space tug. Alter...
Program plans are established for a storable propellant space tug used to perform high energy orbit ...
The feasibility of shuttle orbiter docking to the Space Operations Center (SOC) is studied. The in-o...
Extensively axisymmetric and non-axisymmetric Single Stage To Orbit (SSTO) vehicles are considered. ...
Late in 1990, the NASA Systems Integration Group began functioning and the aircraft systems studies ...
The training requirements of all mission phases for crews and ground support personnel are presented...
The tasks are defined required to design, develop produce, and field support a shuttle mission simul...
Pilot/vehicle analysis techniques for optimizing aircraft handling qualities are presented. The anal...
The work under this grant has been directed to two aspects of the control of flexible spacecraft: (1...
Conceptual design studies were performed directed toward a high power, ultralightweight solar array,...
The Space Station structure has been baselined to be a 5 M (16.4 ft) erectable truss. This structure...
Software conceptual designs (SCD) are presented for meeting the simulator requirements for the shutt...
An outline of the organization and capabilities of the Engine Structures Computational Simulator (Si...
This report discusses the application and cost of two types of altimeter systems (spaceborne (satell...
An experimental flight test program was designed for the Total In Flight Simulator (TIFS) directed t...
Possible storable propellant configurations and program plans are evaluated for the space tug. Alter...
Program plans are established for a storable propellant space tug used to perform high energy orbit ...
The feasibility of shuttle orbiter docking to the Space Operations Center (SOC) is studied. The in-o...
Extensively axisymmetric and non-axisymmetric Single Stage To Orbit (SSTO) vehicles are considered. ...
Late in 1990, the NASA Systems Integration Group began functioning and the aircraft systems studies ...