Studies related to the development of a multiple start-stop solid propellant rocket motor
Multiple start-stop solid propellant rocket motor using highly aluminized ammonium perchlorate annular propellant grains
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Multiple start-stop solid propellant rocket motor using highly aluminized ammonium perchlorate annular propellant grains
Experimental evaluation of gas injection start of Brayton cycle turbocompressor operating on gas bearings
Schematic is provided on a self-starting circuit for a switching regulator which uses a logic circuit to sense a change in output voltage and provides a correction signal for dc power sources. With this device, the total power consumed by the logic circuitry is held to a minimum, and the circuit receives the optimum regulated supply power.
Method which calculates start-up characteristics of centrifugal pumps reveals a capacity to predict pressure drop characteristics of pumps with vaned diffusers. Calculations are based on pump geometry, design-point flow, speed, and pressure rise, and the pump characteristic within range of approximately ten percent of the design-point flow.
Main impulse fields of magnetic storm sudden starts near local absorption region of cosmic radio noise in ionosphere
Factors affecting injection starts of closed-loop single-shaft Brayton power plant
Motor starting characteristics of two inductor alternators
Flow field of impulsively started circular cylinder, noting drag due to nonlinear convection
SNAP 8 sodium potassium pump-motor assembly start tests
Start-up process in gaseous squeeze film thrust bearings
Design and performance of experimental start programmer for SNAP 8 space power system
Suddenly started laminar flow in circular tube entrance region, obtaining integral momentum equation for boundary layer thickness, entrance length, velocity profile, etc
Starting criterion for hypersonic inlets with large turbulent boundary layers, considering total pressure recovery from all shock and viscous losses
Computerized simulation of control systems for nuclear light bulb engine during start-up and at nominal full power operation
Starting circuit design for initiating and maintaining arcs in vapor lamps
Motor-starting characteristics of modified Lundell alternator for single shaft, Brayton cycle, space power system
Motor start of 2 to 10 kilowatt Brayton rotating unit operating on gas bearings in closed loop test facility
Motor starting techniques for 2-15 kW Brayton space power system