Add to ORKGSimulated coasting flight test on sensing tip of liquid-vapor sensor for liquid hydrogen fuel tan
Balloon tank skin strain measurements at liquid hydrogen temperature on Centaur flight vehicl
Future mission planning within NASA continues to include cryogenic propellants for in space transpor...
Frequency and viscous damping of liquids during weightlessness - liquid sloshing characteristics of ...
[Abstract] Liquid-vapor interface detection and liquid mass quantity gauging in capillary-driven sys...
Liquid propellant reorientation experiments in tank models under low level acceleratio
"NASA TM X-1438.""Lewis Research Center, Cleveland, Ohio.""September 1967"--Cover.Includes bibliogra...
Performance testing of liquid-vapor space vehicle sensors in reduced gravity environmen
Motion of liquid-vapor interface in response to imposed acceleration to study behavior of liquid pro...
A test program was conducted involving forty-five drops of liquid propellant in instrumented tanks. ...
Pressure rise characteristics of liquid hydrogen dewar for homogeneous, normal-gravity quiescent, an...
Engineers handbook applicable in prediction of low gravity behavior of liquids in rocket propellant ...
Large amplitude liquid-vapor interface stability in cylinders in response to constant lateral and tr...
Temperature and liquid-level sensor for liquid hydrogen pressurization and expulsion studie
A sensor assembly includes a main body, a sensor, and a filler. The main body includes an outer surf...
Effect of contact angle and space vehicle tank geometry on configuration of rocket propellant liquid...
Balloon tank skin strain measurements at liquid hydrogen temperature on Centaur flight vehicl
Future mission planning within NASA continues to include cryogenic propellants for in space transpor...
Frequency and viscous damping of liquids during weightlessness - liquid sloshing characteristics of ...
[Abstract] Liquid-vapor interface detection and liquid mass quantity gauging in capillary-driven sys...
Liquid propellant reorientation experiments in tank models under low level acceleratio
"NASA TM X-1438.""Lewis Research Center, Cleveland, Ohio.""September 1967"--Cover.Includes bibliogra...
Performance testing of liquid-vapor space vehicle sensors in reduced gravity environmen
Motion of liquid-vapor interface in response to imposed acceleration to study behavior of liquid pro...
A test program was conducted involving forty-five drops of liquid propellant in instrumented tanks. ...
Pressure rise characteristics of liquid hydrogen dewar for homogeneous, normal-gravity quiescent, an...
Engineers handbook applicable in prediction of low gravity behavior of liquids in rocket propellant ...
Large amplitude liquid-vapor interface stability in cylinders in response to constant lateral and tr...
Temperature and liquid-level sensor for liquid hydrogen pressurization and expulsion studie
A sensor assembly includes a main body, a sensor, and a filler. The main body includes an outer surf...
Effect of contact angle and space vehicle tank geometry on configuration of rocket propellant liquid...
Balloon tank skin strain measurements at liquid hydrogen temperature on Centaur flight vehicl
Future mission planning within NASA continues to include cryogenic propellants for in space transpor...
Frequency and viscous damping of liquids during weightlessness - liquid sloshing characteristics of ...