The techniques, processes, and equipment required for automatic fabrication and assembly of structural elements in space using the space shuttle as a launch vehicle and construction base were investigated. Additional construction/systems/operational techniques, processes, and equipment which can be developed/demonstrated in the same program to provide further risk reduction benefits to future large space systems were included. Results in the areas of structure/materials, fabrication systems (beam builder, assembly jig, and avionics/controls), mission integration, and programmatics are summarized. Conclusions and recommendations are given
Facilities are described on which detailed preliminary design was undertaken and which may be used o...
A study was conducted to derive and collect payload information on the anticipated space processing ...
The development effort on the composite beam cap fabricator was completed within cost and close to a...
The techniques, processes, and equipment required for automatic fabrication and assembly of structur...
The performance, design, and verification requirements for the space construction automated fabricat...
The performance, design and verification requirements for the space Construction Automated Fabricati...
The detailed results of all part 3 study tasks are presented. Selected analysis was performed on the...
A range of tasks focused on a baseline system concept is discussed. A beam builder concept developed...
A baseline Space Construction Experiment (SCE) concept is defined. Five characteristics were incorpo...
Definition was completed on a basic flight experiment which will provide data on the construction of...
The essential controls and dynamics community needs for a large space structures is addressed by the...
The implications and impacts devolving upon the orbiter by its utilization as a space construction f...
The fabrication machine used for the rolltrusion and on-orbit forming of graphite thermoplastic (CTP...
Progress in the mechanical/structural assembly of the beam builder is reported. The following struct...
The construction methods specific to the end to end construction process for building the ETVP in lo...
Facilities are described on which detailed preliminary design was undertaken and which may be used o...
A study was conducted to derive and collect payload information on the anticipated space processing ...
The development effort on the composite beam cap fabricator was completed within cost and close to a...
The techniques, processes, and equipment required for automatic fabrication and assembly of structur...
The performance, design, and verification requirements for the space construction automated fabricat...
The performance, design and verification requirements for the space Construction Automated Fabricati...
The detailed results of all part 3 study tasks are presented. Selected analysis was performed on the...
A range of tasks focused on a baseline system concept is discussed. A beam builder concept developed...
A baseline Space Construction Experiment (SCE) concept is defined. Five characteristics were incorpo...
Definition was completed on a basic flight experiment which will provide data on the construction of...
The essential controls and dynamics community needs for a large space structures is addressed by the...
The implications and impacts devolving upon the orbiter by its utilization as a space construction f...
The fabrication machine used for the rolltrusion and on-orbit forming of graphite thermoplastic (CTP...
Progress in the mechanical/structural assembly of the beam builder is reported. The following struct...
The construction methods specific to the end to end construction process for building the ETVP in lo...
Facilities are described on which detailed preliminary design was undertaken and which may be used o...
A study was conducted to derive and collect payload information on the anticipated space processing ...
The development effort on the composite beam cap fabricator was completed within cost and close to a...