Add to ORKGAn improved, reliable method for removing residual hypergolic propellants from Apollo propulsion systems is described . Vapor phase decontamination provides improved efficiency with lower residual contaminant levels , and requir es less time and solvents than liquid flushing . The development and evaluation of this new method is discussed
The wet oxidation process is considered as a potential treatment method for wastes aboard manned spa...
Oxidizer propellant systems for liquid-fueled rocket engines must meet stringent cleanliness require...
Development of gas plasma cleaning technique for removing contaminants from optical surfaces in spac...
Vapor phase cleaning method for Apollo propellant system decontamination and propellant tank dryin
Hardware fabrication and evaluation for trace contaminant removal system integrated with Apollo envi...
Most propulsion systems are designed to be filled and flown, draining can be done but decontaminatio...
Improve method for Apollo propellant system decontamination and propellant tank dryin
An explosive failure of a ground support equipment decontamination unit tank occurred during the pos...
The command module reaction control system is emptied of all remaining propellant using ground suppo...
The efficiency of all treatment methods formerly or currently used in treating chemical wastes is as...
Elimination of permeation and bubble formation in Apollo RCS positive expulsion tankag
Increasingly strict environmental regulations and the consequent phase out of many effective cleanin...
Environmental tests of design modifications for Apollo RCS positive expulsion tankag
Solid rocket propulsion systems have been used for in-space applications including planetary explora...
Alternative techniques for the regeneration of carbon contaminated with various spacecraft contamina...
The wet oxidation process is considered as a potential treatment method for wastes aboard manned spa...
Oxidizer propellant systems for liquid-fueled rocket engines must meet stringent cleanliness require...
Development of gas plasma cleaning technique for removing contaminants from optical surfaces in spac...
Vapor phase cleaning method for Apollo propellant system decontamination and propellant tank dryin
Hardware fabrication and evaluation for trace contaminant removal system integrated with Apollo envi...
Most propulsion systems are designed to be filled and flown, draining can be done but decontaminatio...
Improve method for Apollo propellant system decontamination and propellant tank dryin
An explosive failure of a ground support equipment decontamination unit tank occurred during the pos...
The command module reaction control system is emptied of all remaining propellant using ground suppo...
The efficiency of all treatment methods formerly or currently used in treating chemical wastes is as...
Elimination of permeation and bubble formation in Apollo RCS positive expulsion tankag
Increasingly strict environmental regulations and the consequent phase out of many effective cleanin...
Environmental tests of design modifications for Apollo RCS positive expulsion tankag
Solid rocket propulsion systems have been used for in-space applications including planetary explora...
Alternative techniques for the regeneration of carbon contaminated with various spacecraft contamina...
The wet oxidation process is considered as a potential treatment method for wastes aboard manned spa...
Oxidizer propellant systems for liquid-fueled rocket engines must meet stringent cleanliness require...
Development of gas plasma cleaning technique for removing contaminants from optical surfaces in spac...