Add to ORKGOptimized pressurization system for Apollo-type service module using cryogenic propellant
Mixer design and experimental tank study for cryogenic propellants, with applications for manned Mar...
Proceedings of symposium on cryogenic oxygen storage and supply systems with application to Apollo 1...
Analysis of recirculating type external pressurization systems for use in pressure control of cryoge...
Venting system for use with cryogenic propellants to control tank pressure during zero-gravity coas
Reliquefier design and cycles studied to reduce boiloff in extraterrestrial cryogenic propellant sto...
Selection technique to determine most suitable liquid propellant pressurization systems for various ...
Ignition characteristics and delivered performance of gaseous hydrogen-oxygen reaction control thrus...
An in-depth study and selection of practical propellant surface tension acquisition system designs f...
Lightweight cryogenic He cascade pressurization concept for Apollo service propulsion syste
Design and environmental testing of thermal conditioning unit for liquid hydrogen propellant tan
A review of the design, development, and flight history of the Apollo cryogenic storage system and o...
Comparison of performance of cryogenic propulsion system with earth storable propulsion system for m...
Hybird electronic controller developed for pressurization and venting systems of space propulsion sy...
The development of an acquisition system for supplying subcooled liquid hydrogen and liquid oxygen u...
Ground and vehicle system requirements are evaluated for the use of densified cryogenic propellants ...
Mixer design and experimental tank study for cryogenic propellants, with applications for manned Mar...
Proceedings of symposium on cryogenic oxygen storage and supply systems with application to Apollo 1...
Analysis of recirculating type external pressurization systems for use in pressure control of cryoge...
Venting system for use with cryogenic propellants to control tank pressure during zero-gravity coas
Reliquefier design and cycles studied to reduce boiloff in extraterrestrial cryogenic propellant sto...
Selection technique to determine most suitable liquid propellant pressurization systems for various ...
Ignition characteristics and delivered performance of gaseous hydrogen-oxygen reaction control thrus...
An in-depth study and selection of practical propellant surface tension acquisition system designs f...
Lightweight cryogenic He cascade pressurization concept for Apollo service propulsion syste
Design and environmental testing of thermal conditioning unit for liquid hydrogen propellant tan
A review of the design, development, and flight history of the Apollo cryogenic storage system and o...
Comparison of performance of cryogenic propulsion system with earth storable propulsion system for m...
Hybird electronic controller developed for pressurization and venting systems of space propulsion sy...
The development of an acquisition system for supplying subcooled liquid hydrogen and liquid oxygen u...
Ground and vehicle system requirements are evaluated for the use of densified cryogenic propellants ...
Mixer design and experimental tank study for cryogenic propellants, with applications for manned Mar...
Proceedings of symposium on cryogenic oxygen storage and supply systems with application to Apollo 1...
Analysis of recirculating type external pressurization systems for use in pressure control of cryoge...