Excitation temperature of the 18-cm line of OH in H I regions.
Excitation temperature of 18 cm line of OH in H 1 clouds, discussing excitation mechanisms and OH/H abundance ratios
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Excitation temperature of 18 cm line of OH in H 1 clouds, discussing excitation mechanisms and OH/H abundance ratios
Direct and autoionization of H molecule by electron impact near threshold noting cross section, photoionization and vibrational and rotational energy changes
Solar flares recorded by Lyot H alpha heliograph /1958-1965/, discussing flare distribution
Solar flares compilation and properties analysis from Cape of Good Hope Lyot H alpha heliograph observations /1958-1965/
Natural orbital expansion coefficients of LCAO-MO-SCF-CI wave functions for ground state of H molecule
Resonance effects between H levels by induced electric dipole transitions, using spatially periodic potential barriers
Stark broadening of H-gamma for electron density measurement in plasma, noting temperature range
Deuterium atom reaction with hydrogen molecule yielding HD and H using modulated crossed beams, plotting angular distributions and reaction velocities
Solar Ca II H and K lines formation, discussing double reversal, limb darkening, plage and spot lines and anomalous line ratios
H alpha filtergrams of sun during solar eclipse of 7 March 1970, showing bright plage area
Time and power dependent Lamb shift resonance shapes measurement with circular polarized RF field in beam foil excited H atoms
H alpha flares occurrence in plages with little or no spots
Stark induced quantum beats in H Ly alpha emission, using beam foil excited hydrogen
Low energy cosmic ray H 2 and He 3 nuclei intensities /1967-1968/ from Pioneer 8 and IMP 4 measurements
Type 3 solar radio bursts in absence of H alpha flares, noting soft X-ray emission
Limiting He 3 abundances in four H II regions
Venus upper atmospheric UV spectra from rocket- borne telescope spectrophotometer, considering O I and H I emission features
Experimental aerodynamic investigations were made in the Grumman 36-inch hypersonic wind tunnel on a .00435 scale model of the H-32 reusable space shuttle booster. The objectives of the test were to determine the static stability characteristics and control surface effectiveness at hypersonic speeds. Data were taken at M = 8.12 over a range of angles of attack between -5 and 85 deg at beta = 0 deg and over a range of side slip angles between -10 and 10 deg at alpha = 0 and 70 deg. Six component balance data and base-cavity pressure data were recorded.