Add to ORKGThe following subject areas are covered: background (space propulsion facility assessment team final report); changes (Advanced Launch System, National Aerospace Plane, and space exploration initiative); life cycle cost analysis rationale; and recommendation to panel
The information management system (IMS) special emphasis task was performed as an adjunct to the mod...
The use of lunar surface photography to achieve the photogrammetric transfer of available selenograp...
Gravity gradient stabilization is planned for the space station. Torques arise from air-drag since t...
As a result of high cycle fatigue, hydrogen embrittlement, and extended engine use, it was observed ...
The guidelines for EVA and IVA tasks to be performed on the space shuttle are defined. In deriving t...
This study was initiated to identify operations problems and cost drivers for current propulsion sys...
Asymptotic formulas for the characteristic root errors as well as transfer function gain and phase e...
Given here are the proceedings of the 3rd Space Exploration Initiative (SEI) Technical Interchange. ...
Two important aspects of concurrent processing under development at TRW are discussed. These are: (1...
In Jan. 1991, the LaRc SSFO performed an assessment of the configuration characteristics of the prop...
The requirements for space shuttle emergency intravehicular activity support equipment are discussed...
This document presents an overview of the characteristics and capabilities of the flight telerobotic...
The Space Station structure has been baselined to be a 5 M (16.4 ft) erectable truss. This structure...
The SAFT prismatic VOS Ni-Cd cells have been flown in geosynchronous orbit since 1977 and in low ear...
Film/dump cooling a rocket nozzle with fuel rich gas, as in the National Launch System (NLS) Space T...
The information management system (IMS) special emphasis task was performed as an adjunct to the mod...
The use of lunar surface photography to achieve the photogrammetric transfer of available selenograp...
Gravity gradient stabilization is planned for the space station. Torques arise from air-drag since t...
As a result of high cycle fatigue, hydrogen embrittlement, and extended engine use, it was observed ...
The guidelines for EVA and IVA tasks to be performed on the space shuttle are defined. In deriving t...
This study was initiated to identify operations problems and cost drivers for current propulsion sys...
Asymptotic formulas for the characteristic root errors as well as transfer function gain and phase e...
Given here are the proceedings of the 3rd Space Exploration Initiative (SEI) Technical Interchange. ...
Two important aspects of concurrent processing under development at TRW are discussed. These are: (1...
In Jan. 1991, the LaRc SSFO performed an assessment of the configuration characteristics of the prop...
The requirements for space shuttle emergency intravehicular activity support equipment are discussed...
This document presents an overview of the characteristics and capabilities of the flight telerobotic...
The Space Station structure has been baselined to be a 5 M (16.4 ft) erectable truss. This structure...
The SAFT prismatic VOS Ni-Cd cells have been flown in geosynchronous orbit since 1977 and in low ear...
Film/dump cooling a rocket nozzle with fuel rich gas, as in the National Launch System (NLS) Space T...
The information management system (IMS) special emphasis task was performed as an adjunct to the mod...
The use of lunar surface photography to achieve the photogrammetric transfer of available selenograp...
Gravity gradient stabilization is planned for the space station. Torques arise from air-drag since t...