The hydraulic characteristics of flow through miniature slot orifices
Hydraulic characteristics of flow through miniature slot orifices for rocket engine injectors
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Hydraulic characteristics of flow through miniature slot orifices for rocket engine injectors
Turbopump weight minimization and low suction pressure requirements realized using high rotating speeds, hydraulic turbine driven upstream inducer and computer testing
Transient performance of full flow hydraulic turbine driven two speed pump inducer system, formulating computer model
Hydraulic-powered self propelled six degree of freedom loading vehicle moving tests assembly to test chamber with high accuracy positioning
Hydraulic characteristics of micro-orifices arrayed in close proximity across the face of a liquid fuel injector are studied. Effects of geometry and flow variables on discharge coefficients and flow regimes are determined, as well as visible characteristics of the emerging liquid streams.
Turbine, driven by the fluid being pumped, requires no external controls, is completely integrated into the flow system, and has bearings which utilize the main fluid for lubrication and cooling. Torque capabilities compare favorably with those developed by positive displacement hydraulic motors.
Detection of malfunctions in hydraulic components of antenna drives and means for acquisition, processing and interpretation of diagnostic data
Techniques and applications of fluid-control devices and hydraulic components
Minimum cleanliness levels for pneumatic and hydraulic systems on Launch Complex 39 service arms of Saturn 5
Control techniques for simultaneous three degree of freedom hydraulic vibration system
Hydraulic fluid analysis for reducing wear, and detection of component failure
Diagnostic, testing, and maintenance procedures for hydraulic drive systems for large steerable antennas
High temperature polyimide actuator rod seals for aircraft hydraulic systems
Small three stage hydraulic turbine for aerospace and commercial applications, discussing design and performance
Hydraulic characteristics of flow through miniature slot orifices for rocket engine injectors, observing stability of effluent liquid streams
Spacecraft hydraulic timers design and qualifications testing, discussing oil selection and temperature dependence
Two types of polyimide seals are developed for hydraulic actuator rod in low pressure second stage of two-stage configuration. Each seal melts test objectives of twenty million cycles of operation at 534 K. Analytical and experimental study results are discussed. Potential applications are given.
Hydraulic support apparatus for dynamic testing of space vehicles under near-free flight conditions