Design details and test results of the jet-centrifugal mercury pump are presented. (auth
The SNAP I development program was initiated to develop a 500-watt turboelectric power conversion sy...
The 3 kw nuclear auxiliary power unit deslgnated SNAP II is intended for use in a satellite vehicle....
The SNAP II boilers which were designed are summarized. As shown by test results from the three boil...
BS>SNAP II is the designation for a 3 kw nuclear auxiliary power unii for utilization in a satellite...
SNAP 1 is the designation for the 0.5-kw nuclear auxiliary power supply intended for application in ...
S>Pump development for the SNAP I power conversion system is described. A four-vaned impeller pump s...
The mercury-boiler development program was undertaken to develop a system that would utilize the hea...
An electromagnetic pump, in which pressure is developed in mercury because of the interaction of the...
SNAP II is the designation for a 3-kw nuclear auxiliary power untt to be used in a satellite vehicle...
The mercury-boiler development program was undertaken to develop a system that would utilize the hea...
Boiling and condensing experiments under zero gravity conditions were conducted to investigate the o...
SNAP II is the designation for a 3 kw nuclear auxiliary power unit to be used in a satellite vehicle...
A compact electromagnetic pump utilizing a rotating permanent magnet with radial gap was developed f...
Investigations of materials for use in connection with the SNAP I mercury Rankine cycle power conver...
Development of bearings for use in the SNAP I power conversion system is described. Liquid mercury, ...
The SNAP I development program was initiated to develop a 500-watt turboelectric power conversion sy...
The 3 kw nuclear auxiliary power unit deslgnated SNAP II is intended for use in a satellite vehicle....
The SNAP II boilers which were designed are summarized. As shown by test results from the three boil...
BS>SNAP II is the designation for a 3 kw nuclear auxiliary power unii for utilization in a satellite...
SNAP 1 is the designation for the 0.5-kw nuclear auxiliary power supply intended for application in ...
S>Pump development for the SNAP I power conversion system is described. A four-vaned impeller pump s...
The mercury-boiler development program was undertaken to develop a system that would utilize the hea...
An electromagnetic pump, in which pressure is developed in mercury because of the interaction of the...
SNAP II is the designation for a 3-kw nuclear auxiliary power untt to be used in a satellite vehicle...
The mercury-boiler development program was undertaken to develop a system that would utilize the hea...
Boiling and condensing experiments under zero gravity conditions were conducted to investigate the o...
SNAP II is the designation for a 3 kw nuclear auxiliary power unit to be used in a satellite vehicle...
A compact electromagnetic pump utilizing a rotating permanent magnet with radial gap was developed f...
Investigations of materials for use in connection with the SNAP I mercury Rankine cycle power conver...
Development of bearings for use in the SNAP I power conversion system is described. Liquid mercury, ...
The SNAP I development program was initiated to develop a 500-watt turboelectric power conversion sy...
The 3 kw nuclear auxiliary power unit deslgnated SNAP II is intended for use in a satellite vehicle....
The SNAP II boilers which were designed are summarized. As shown by test results from the three boil...