Observations of the anomalous microwave recombination line at 11 cm wavelength
Anomalous microwave recombination line at 11 cm detected in NGC 2024, Orion A, and IC 1795, discussing peak antenna temperature
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Anomalous microwave recombination line at 11 cm detected in NGC 2024, Orion A, and IC 1795, discussing peak antenna temperature
Polarized and depolarized radar maps of moon, attributing anomalies and average diffuse component of echoes to scattering behavior of surface and subsurface rocks
Millimeter wave and optical astronomical refraction differential measurements, showing dependence on atmospheric water vapor
Ion acoustic wave propagation in collisionless gravity-supported plasma in static magnetic field calculated from linearized Vlasov equation
Process obtains solar heating data which support analytical design. Process yields quantitative information on local solar exposure of models which are geometrically and reflectively similar to prototypes under study. Models are tested in a shirtsleeve environment.
Development of electromagnetic wave transmission line circulator and application to parametric amplifier circuits
Amino acids produced by long UV irradiation of gas mixtures using hydrogen sulfide as initial photon acceptor, simulating prebiological earth conditions
Celestial sources far IR radiation detection using balloon-borne telescope
Fluoride overcoated Al reflectance measurements and polarization effects at various angles of incidence, noting utilization in vacuum UV instrumentation
Polarized solar millimeter emission associated with sunspot magnetic field compatible with multiple sources from chromosphere
Methyl alcohol transitions in Orion at 1 cm noting emission source coincidence with IR nebula
Optical phonons and temperature dependent phase transitions in paraelectric antimony and ferroelectric sulfoiodide semiconductors, using polarized IR and Raman spectra measurements
Carbon dioxide photolysis at 1740-2100 A applied to photochemistry of Mars lower atmosphere
Fabry-Perot interferometer measurements of atomic oxygen 6300 A and 5577 A line profiles from twilight and nightglow are used to determine the neutral temperatures in F2 and E regions of the earth's ionosphere. The exospheric temperatures T sub n (infinity) determined from the 6300 A profiles are usually somewhat higher than those calculated from Jacchia's model, with differences as large as approximately 300 K noted when T sub n (infinity) = 1500 to 1600 K. The post-sunset and pre-dawn rate of change of T sub n (infinity) is often substantially larger than the Jacchia prediction. The 5577 A (E-region) measured temperatures range from 200 to 220 K on quiet nights to 500 to 600 K during geomagnetic storms.
Measurements in five different passbands in the spectral region below 20/cm were made with a liquid helium-cooled radiometer in two flights at approximately 40 km altitude. The equivalent temperatures are given for passbands of 1 to 5.4, 7.8, 7.9, 11.1, and 18.5/cm. The results are consistent with a 2.7 K thermal radiation background. Atmospheric radiation of uncertain magnitude dominates the region above 11/cm.
The relative dielectric constant and loss tangent of lunar sample 14163,164 (fine dust) were determined as a function of density at 9.375, 24, 35, and 60 GHz. In addition, such measurements have also been performed on lunar sample 14310,74 (solid rock) at 9.375 GHz. The loss tangent was found to be frequency independent at these test frequencies and had a value of 0.015 for the lunar dust sample.
The ways in which radio signals are affected by meteorological parameters are described, as are methods for interpreting the signals, the state-of-the-art in instrumentation, the current state of development of the field, and some problems and prospects for the future. It is shown that the temperature profile of the atmosphere, water vapor and ozone distribution, cloud water content, and certain surface properties can be measured with sufficient accuracy to provide useful meteorological information.
Rocket studies of the low-energy X-ray sky conducted so far suffer from serious experimental problems. Therefore, an apparatus was design ed to overcome the outstanding experimental problems. The instrument developed was successfully flown in an Aerobee-170 rocket. The new device utilizes a grazing incidence paraboloid as an energy concentrator and low-pass filter. The effective bandpass of the instrument from 100 to 280 eV is determined by the combination of the counter window transmission and the mirror reflectivity.