This study was initiated to identify operations problems and cost drivers for current propulsion systems and to identify technology and design approaches to increase the operational efficiency and reduce operations costs for future propulsion systems. To provide readily usable data for the Advanced Launch System (ALS) Program, the results of the Operationally Efficient Propulsion System Study (OEPSS) were organized into a series of OEPSS Data Books. This volume contains the final briefing on the OEPSS first-year effort. This briefing was presented to MSFC as part of an effort to promote greater interaction between the design community and the launch site operator
Extensively axisymmetric and non-axisymmetric Single Stage To Orbit (SSTO) vehicles are considered. ...
Gravity gradient stabilization is planned for the space station. Torques arise from air-drag since t...
The topics addressed are: (1) Terminal Doppler Weather Radar (TDWR) 1991 program review; (2) TDWR de...
In Jan. 1991, the LaRc SSFO performed an assessment of the configuration characteristics of the prop...
The guidelines for EVA and IVA tasks to be performed on the space shuttle are defined. In deriving t...
This document presents an overview of the characteristics and capabilities of the flight telerobotic...
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. ...
Asymptotic formulas for the characteristic root errors as well as transfer function gain and phase e...
The Space Station structure has been baselined to be a 5 M (16.4 ft) erectable truss. This structure...
Film/dump cooling a rocket nozzle with fuel rich gas, as in the National Launch System (NLS) Space T...
As a result of high cycle fatigue, hydrogen embrittlement, and extended engine use, it was observed ...
The information management system (IMS) special emphasis task was performed as an adjunct to the mod...
Information is given in viewgraph form on advanced flight software reconfiguration. Reconfiguration ...
The development process of the knowledge base for the generation of Test Libraries for Mission Opera...
Extensively axisymmetric and non-axisymmetric Single Stage To Orbit (SSTO) vehicles are considered. ...
Gravity gradient stabilization is planned for the space station. Torques arise from air-drag since t...
The topics addressed are: (1) Terminal Doppler Weather Radar (TDWR) 1991 program review; (2) TDWR de...
In Jan. 1991, the LaRc SSFO performed an assessment of the configuration characteristics of the prop...
The guidelines for EVA and IVA tasks to be performed on the space shuttle are defined. In deriving t...
This document presents an overview of the characteristics and capabilities of the flight telerobotic...
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. ...
Asymptotic formulas for the characteristic root errors as well as transfer function gain and phase e...
The Space Station structure has been baselined to be a 5 M (16.4 ft) erectable truss. This structure...
Film/dump cooling a rocket nozzle with fuel rich gas, as in the National Launch System (NLS) Space T...
As a result of high cycle fatigue, hydrogen embrittlement, and extended engine use, it was observed ...
The information management system (IMS) special emphasis task was performed as an adjunct to the mod...
Information is given in viewgraph form on advanced flight software reconfiguration. Reconfiguration ...
The development process of the knowledge base for the generation of Test Libraries for Mission Opera...
Extensively axisymmetric and non-axisymmetric Single Stage To Orbit (SSTO) vehicles are considered. ...
Gravity gradient stabilization is planned for the space station. Torques arise from air-drag since t...
The topics addressed are: (1) Terminal Doppler Weather Radar (TDWR) 1991 program review; (2) TDWR de...