Evaluation of acoustic cavities for combustion stabilization Final report, 30 Jun. 1969 - 30 Jan. 1971
Stabilizing influence of acoustic cavities on acoustic modes of combustion instability in rocket engines
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Stabilizing influence of acoustic cavities on acoustic modes of combustion instability in rocket engines
Power level variations in cavity reactor produced by density changes in gaseous nuclear fuels
Fuel wave formation and control in coaxial flowing gas cavity reactor for space nuclear propulsion
Mockup of coaxial flowing gas cavity reactor for space nuclear propulsion, performed with critical experiment
Critical mass experiments to establish design calculation standards for modular cavity reactors of gas core nuclear rocket engines
Propulsion and weight analyses of mini-cavity reactor rocket engine concept
Nozzle and cavity wall cooling limitations on specific impusle of gas-core nuclear rocket engine
NASTRAN program used to calculate stress concentration caused by surface cavities in plates under biaxial loading
Adaptation of NASTRAN program to solve acoustic mode problems of solid rocket motor cavities by finite element method
Single frequency carbon dioxide laser cavity length computer aided selection for reduced line competition, considering heterodyne communications systems
Postcoupled waveguide cavity Gunn effect microwave oscillator equivalent circuit analysis, using lumped constant elements
Waveguide cavity CW Gunn microwave oscillator bias voltage controlled amplitude and frequency modulation
Lunar diamagnetic cavity signatures from Ames magnetometer experiment on Explorer 35 orbiter, indicating solar wind interaction
Field components, frequency, quality and filling factors effects of storage quartz bulbs in maser microwave cavities
Active cavity radiometric and international pyrheliometric scales comparison and solar constant from simultaneous solar irradiance measurements
Degasser, a cylindrical container made of plastic thick enough to withstand operating pressures of electrolysis module, removes accumulated gases from water cavities without loss of electrolyte.
New type cavity resonator is designed for hydrogen maser. Resonator consists of three pieces of glass-ceramic material having extremely low thermal coefficient of expansion and provides very stable mechanical tuning.
The equations of motion used in the computation are discussed along with the space charge fields and the integration process. The following assumptions were used as a basis for the computation: (1) The beam is divided into N axisymmetric discs of equal charge and each disc into R rings of equal charge. (2) The velocity of each disc, its phase with respect to the gap voltage, and its radius at a specified position in the drift tunnel prior to the interaction gap is known from available large signal one dimensional programs. (3) The fringing rf fields are computed from exact analytical expressions derived from the wave equation assuming a known field shape between the tunnel tips at a radius a. (4) The beam is focused by an axisymmetric magnetic field. Both components of B, that is B sub z and B sub r, are taken into account. (5) Since this integration does not start at the cathode but rather further down the stream prior to entering the output cavity it is assumed that each electron moved along a laminar path from the cathode to the start of integration.