Add to ORKGA review of the design, development, and flight history of the Apollo cryogenic storage system and of selected components within the system is presented. Discussions are presented on the development history of the pressure vessels, heaters, insulation, and selected components. Flight experience and operational difficulties are reported in detail to provide definition of the problems and applicable corrective actions
The development of an acquisition system for supplying subcooled liquid hydrogen and liquid oxygen u...
The conceptual design of a Spacelab cryogen management experiment was performed to demonstrate toe d...
An in-depth study and selection of practical propellant surface tension acquisition system designs f...
An assessment of the Apollo 13 mission resulted in establishing new and revised requirements for the...
Proceedings of symposium on cryogenic oxygen storage and supply systems with application to Apollo 1...
Optimized pressurization system for Apollo-type service module using cryogenic propellant
The integrated systems program is capable of simulating both nominal and anomalous operation of the ...
Cryogenic gas storage systems were developed for the liquid storage of oxygen, hydrogen, nitrogen, a...
The Apollo 13 anomaly provided considerable impetus for a variety of types of cryogenic and ignition...
Electric power generation and cryogenic gas storage systems for Apollo applications program mission ...
The development and performance history of the Apollo extravehicular mobility unit and its major sub...
Vessel and shell fabrication, prototype thermal, and structural models, and cryogenic vessel thermal...
A comprehensive review is presented of the design philosophy of the Apollo environmental control sys...
The design and development of cryogenic supply systems for space shuttle vehicles are discussed. The...
Physical, metallurgical, chemical, and thermodynamic surveys of high pressure tanks and plumbing sys...
The development of an acquisition system for supplying subcooled liquid hydrogen and liquid oxygen u...
The conceptual design of a Spacelab cryogen management experiment was performed to demonstrate toe d...
An in-depth study and selection of practical propellant surface tension acquisition system designs f...
An assessment of the Apollo 13 mission resulted in establishing new and revised requirements for the...
Proceedings of symposium on cryogenic oxygen storage and supply systems with application to Apollo 1...
Optimized pressurization system for Apollo-type service module using cryogenic propellant
The integrated systems program is capable of simulating both nominal and anomalous operation of the ...
Cryogenic gas storage systems were developed for the liquid storage of oxygen, hydrogen, nitrogen, a...
The Apollo 13 anomaly provided considerable impetus for a variety of types of cryogenic and ignition...
Electric power generation and cryogenic gas storage systems for Apollo applications program mission ...
The development and performance history of the Apollo extravehicular mobility unit and its major sub...
Vessel and shell fabrication, prototype thermal, and structural models, and cryogenic vessel thermal...
A comprehensive review is presented of the design philosophy of the Apollo environmental control sys...
The design and development of cryogenic supply systems for space shuttle vehicles are discussed. The...
Physical, metallurgical, chemical, and thermodynamic surveys of high pressure tanks and plumbing sys...
The development of an acquisition system for supplying subcooled liquid hydrogen and liquid oxygen u...
The conceptual design of a Spacelab cryogen management experiment was performed to demonstrate toe d...
An in-depth study and selection of practical propellant surface tension acquisition system designs f...