ASD Technical Report, Numéro 63,Partie 834Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1964 |
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Table des matières
INTRODUCTION AND SUMMARY | 1 |
POLY PHASE POWER SOURCE | 31 |
IONIZATION AND ACCELERATION OF GAS | 51 |
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Expressions et termes fréquents
4th IPA acceleration process accelerator gun air mass delivery amperes amperes peak-to-peak background pressure ballistic pendulum Block Diagram carrier frequency Class C Grid conduction angle cooling cryogenic pumping system cryopump designed and built diagnostic diameter diffusion pump electric electrode expansion ferrite material field velocity Figure 22 Figure 28a FLIGHT DYNAMICS flow rate fourth IPA gas injector gauges gr/sec grams per second heat exchanger helium inches inductance injected input Ionized Argon Beam ions kc/sec L2 and L3 liquid nitrogen magnetic field meters nozzle peak-to-peak phase photograph pitot tube PLASMA ACCELERATOR plate power amplifier power source power supply PRINCIPLE OF OPERATION probe pyrex RELAY resonant frequency ring currents rod of ferrite roughing pump Schmidt trigger shown in Figure Shunt Modulator signal speed taken by Camera tank circuit TBC-3 Transmitter thermocouple Three-Phase Oscillator Torr traveling field traveling wave tube tuning capacitors turbine vacuum chamber vacuum envelope valve voltage wavelength