The overall purpose of the Electrolysis Performance Improvement Concept Study flight experiment is to demonstrate and validate in a microgravity environment the Static Feed Electrolyzer concept as well as investigate the effect of microgravity on water electrolysis performance. The scope of the experiment includes variations in microstructural characteristics of electrodes and current densities in a static feed electrolysis cell configuration. The results of the flight experiment will be used to improve efficiency of the static feed electrolysis process and other electrochemical regenerative life support processes by reducing power and expanding the operational range. Specific technologies that will benefit include water electrolysis for pr...
Economic studies were conducted for three general fuel conserving options: (1) improving fuel consum...
A biological system proposed to restrain a monkey in the Spacelab was tested under operational condi...
The Remote Field Eddy Current (RFEC) technique is ideal for inspecting unpiggable pipelines because ...
Attitude control is reviewed, encompassing the attitude control subsystem, spacecraft attitude preci...
Prototype space flight experiment package for study of circadian periodicity in pocket mic
The objective of this program is to develop generic load models with multiple levels of progressive ...
This final report describes work performed by SRS Technologies for the NASA Marshall Space Flight Ce...
Advanced high performance vehicles, including Single-Stage-To-Orbit (SSTO) hypersonic flight vehicle...
Multicomputer configurations and redundancy management techniques used in various airborne systems w...
The Oak Ridge National Laboratory (ORNL) Laboratory Directed Research and Development (LDRD) Program...
The Advanced Cockpit Controls/Advanced Flight Control System (ACC/AFCS) study was conducted by the B...
The Oak Ridge National Laboratory (ORNL) Laboratory Directed Research and Development (LDRD) Program...
The scope of the study is to investigate ways of controlling the microgravity environment of the Int...
Activity conducted in the following areas is highlighted: space sciences, space transportation syste...
Conceptual design study of advanced Mariner space probe - flyby bus design for Mars missio
Economic studies were conducted for three general fuel conserving options: (1) improving fuel consum...
A biological system proposed to restrain a monkey in the Spacelab was tested under operational condi...
The Remote Field Eddy Current (RFEC) technique is ideal for inspecting unpiggable pipelines because ...
Attitude control is reviewed, encompassing the attitude control subsystem, spacecraft attitude preci...
Prototype space flight experiment package for study of circadian periodicity in pocket mic
The objective of this program is to develop generic load models with multiple levels of progressive ...
This final report describes work performed by SRS Technologies for the NASA Marshall Space Flight Ce...
Advanced high performance vehicles, including Single-Stage-To-Orbit (SSTO) hypersonic flight vehicle...
Multicomputer configurations and redundancy management techniques used in various airborne systems w...
The Oak Ridge National Laboratory (ORNL) Laboratory Directed Research and Development (LDRD) Program...
The Advanced Cockpit Controls/Advanced Flight Control System (ACC/AFCS) study was conducted by the B...
The Oak Ridge National Laboratory (ORNL) Laboratory Directed Research and Development (LDRD) Program...
The scope of the study is to investigate ways of controlling the microgravity environment of the Int...
Activity conducted in the following areas is highlighted: space sciences, space transportation syste...
Conceptual design study of advanced Mariner space probe - flyby bus design for Mars missio
Economic studies were conducted for three general fuel conserving options: (1) improving fuel consum...
A biological system proposed to restrain a monkey in the Spacelab was tested under operational condi...
The Remote Field Eddy Current (RFEC) technique is ideal for inspecting unpiggable pipelines because ...