This document presents an overview of the characteristics and capabilities of the flight telerobotic servicer (FTS), under development at GSFC at the time the report was prepared; the project has since been cancelled. The assessment was directed toward developing the FTS to enable assembly and servicing of the Mars vehicle at the space station; facilitate rendezvous, docking, and fluid transfer operations involving the Mars vehicle fuel tank; to perform strip-mining operations on the lunar/martian surfaces; and to construct a three-story shelter on the martian surface. The report considers the FTS' mechanical, electrical, thermal, and operational subsystems, as well as its proposed manipulator capabilities
To support the reusable launch vehicle concept study, the aerodynamic data and surface pressure for ...
The SAFT prismatic VOS Ni-Cd cells have been flown in geosynchronous orbit since 1977 and in low ear...
The following subject areas are covered: background (space propulsion facility assessment team final...
In Jan. 1991, the LaRc SSFO performed an assessment of the configuration characteristics of the prop...
The Space Station structure has been baselined to be a 5 M (16.4 ft) erectable truss. This structure...
This study was initiated to identify operations problems and cost drivers for current propulsion sys...
Two important aspects of concurrent processing under development at TRW are discussed. These are: (1...
Given here are the proceedings of the 3rd Space Exploration Initiative (SEI) Technical Interchange. ...
Information is given in viewgraph form on advanced flight software reconfiguration. Reconfiguration ...
The guidelines for EVA and IVA tasks to be performed on the space shuttle are defined. In deriving t...
As a result of high cycle fatigue, hydrogen embrittlement, and extended engine use, it was observed ...
Asymptotic formulas for the characteristic root errors as well as transfer function gain and phase e...
Three-dimensional, conjugate (solid/fluid) heat transfer analyses of new designs of the Solid Rocket...
Early space station accommodation, build-up of space station manipulator capability, on-orbit spacec...
General servicing requirements, a servicing mission concept and scenario, overall servicing needs, b...
To support the reusable launch vehicle concept study, the aerodynamic data and surface pressure for ...
The SAFT prismatic VOS Ni-Cd cells have been flown in geosynchronous orbit since 1977 and in low ear...
The following subject areas are covered: background (space propulsion facility assessment team final...
In Jan. 1991, the LaRc SSFO performed an assessment of the configuration characteristics of the prop...
The Space Station structure has been baselined to be a 5 M (16.4 ft) erectable truss. This structure...
This study was initiated to identify operations problems and cost drivers for current propulsion sys...
Two important aspects of concurrent processing under development at TRW are discussed. These are: (1...
Given here are the proceedings of the 3rd Space Exploration Initiative (SEI) Technical Interchange. ...
Information is given in viewgraph form on advanced flight software reconfiguration. Reconfiguration ...
The guidelines for EVA and IVA tasks to be performed on the space shuttle are defined. In deriving t...
As a result of high cycle fatigue, hydrogen embrittlement, and extended engine use, it was observed ...
Asymptotic formulas for the characteristic root errors as well as transfer function gain and phase e...
Three-dimensional, conjugate (solid/fluid) heat transfer analyses of new designs of the Solid Rocket...
Early space station accommodation, build-up of space station manipulator capability, on-orbit spacec...
General servicing requirements, a servicing mission concept and scenario, overall servicing needs, b...
To support the reusable launch vehicle concept study, the aerodynamic data and surface pressure for ...
The SAFT prismatic VOS Ni-Cd cells have been flown in geosynchronous orbit since 1977 and in low ear...
The following subject areas are covered: background (space propulsion facility assessment team final...