Programmatic benefits to payloads are examined which can result from the routine use of extravehicular activity (EVA) during space missions. Design and operations costs were compared for 13 representative baseline payloads to the costs of those payloads adapted for EVA operations. The EVA-oriented concepts developed in the study were derived from these baseline concepts and maintained mission and program objectives as well as basic configurations. This permitted isolation of cost saving factors associated specifically with incorporation of EVA in a variety of payload designs and operations. The study results were extrapolated to a total of 74 payload programs. Using appropriate complexity and learning factors, net EVA savings were extrapola...
Requirements are projected for performing orbital satellite service. Emphasis is on defining the rol...
The orbiter/payload interface area was examined with respect to integrating the payload to the shutt...
The study examined impacts of changing Orbiter cabin pressure and EMU EVA pressure to eliminate pure...
Descriptions of the EVA system baselined for the space shuttle program were provided, as well as a c...
The development of a model for estimating the impact of manned EVA costs on future payloads is discu...
Parameters that require consideration by the planners and designers when planning for man to perform...
A technology assessment is presented on space extravehicular activities (EVA) that will be possible ...
Several EV workstation concepts were developed and are documented. The workstation concepts were dev...
EVA equipment design guides and crewman interfaces are provided. A summary presents data on suited c...
EVA crewman/equipment translational concepts are developed for a shuttle orbiter payload application...
Research was conducted to provide data on ways to effectively realize the projected cost reductions ...
The goal of NASA s current EVA technology effort is to further develop technologies that will be use...
Potential modes of operating in space in the space shuttle era are documented. The October 1973 NASA...
The objectives of this presentation are to: Define Extravehicular Activity (EVA), identify the reaso...
Subjects related to future STS operations concepts were investigated. The majority of effort was dir...
Requirements are projected for performing orbital satellite service. Emphasis is on defining the rol...
The orbiter/payload interface area was examined with respect to integrating the payload to the shutt...
The study examined impacts of changing Orbiter cabin pressure and EMU EVA pressure to eliminate pure...
Descriptions of the EVA system baselined for the space shuttle program were provided, as well as a c...
The development of a model for estimating the impact of manned EVA costs on future payloads is discu...
Parameters that require consideration by the planners and designers when planning for man to perform...
A technology assessment is presented on space extravehicular activities (EVA) that will be possible ...
Several EV workstation concepts were developed and are documented. The workstation concepts were dev...
EVA equipment design guides and crewman interfaces are provided. A summary presents data on suited c...
EVA crewman/equipment translational concepts are developed for a shuttle orbiter payload application...
Research was conducted to provide data on ways to effectively realize the projected cost reductions ...
The goal of NASA s current EVA technology effort is to further develop technologies that will be use...
Potential modes of operating in space in the space shuttle era are documented. The October 1973 NASA...
The objectives of this presentation are to: Define Extravehicular Activity (EVA), identify the reaso...
Subjects related to future STS operations concepts were investigated. The majority of effort was dir...
Requirements are projected for performing orbital satellite service. Emphasis is on defining the rol...
The orbiter/payload interface area was examined with respect to integrating the payload to the shutt...
The study examined impacts of changing Orbiter cabin pressure and EMU EVA pressure to eliminate pure...