Particle acceleration in low-power hotspots: modelling the broad-band spectral energy distribution
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Satellite orbital transfer using arc-jet engine - electrothermal propulsion systems
High power drain is eliminated by a circuit consisting of a divide-by-two stage, two identical inputs, a wiggle amplifier, driver, and power output stages to drive the step motor.
Magnetic, thin-film, plated-wire spacecraft memory
Performance data of resistojet designed for attitude control and station keeping of 500-lb synchronous satellite
Two-kw continuous arc jet thrustor for spacecraft attitude control, orbit maintenance and orbit transfer
Two-transistor multivibrator has minimum power dissipation and maximum reliability. It minimizes the use of components that are subject to environmental changes or other unpredictable behavior.
Timing device for controlling camera shutter during Aerobee rocket flight
Inverter with integrated components and direct coupled inverter circuit not needing transformers for space applications
Consumption multichannel pulse height analyzer performs balloon and rocket investigations of solar neutrons with energies greater than 10 MeV. The lightweight unit can operate in a temperature range of minus 30 degrees to plus 70 degrees C and withstand storage temperatures from minus 50 degrees to plus 90 degrees C.
This paper describes a device for timing sequentially 8 film exposures of a rocket-borne camera with a time interval between each exposure to allow the camera film transport mechanism to step the film from one frame to the next after each exposure. Each exposure time can be independently adjusted from a a fraction of a second to several hundred seconds by changing the value of a timing resistor and/or capacitor. All of the rocket interface circuits have ben designed to minimize the coupling of spurious noise signals into the timer.
Silicon switching transistor with saturation voltage of 0.1 V at 75 A collector current
A regulated dc-to-dc converter requires negligible standby power for the operation of critical electronic equipment. The main operating circuitry consumes power intermittently according to load conditions, rather than constantly.
Gimbaled spinmotor, gyro assembly, and gyro test results for gas bearing gyroscopes with high G and sterilization capability
Preliminary assembly and initial test results of gas bearing gyroscope with high-g and sterilization capabilities
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