Some results of rocket experiments in the quiet d region
Electron density profiles for quiet day mid- latitude d region using nike-apache sounding rockets
Engineering topics
Publications and source records attributed to Kane, J. A..
Electron density profiles for quiet day mid- latitude d region using nike-apache sounding rockets
Rocket measurement of electron density in low ionosphere
Midlatitude electron density profile in d region indicating nitric oxide ionization by lyman alpha radiation
Rocket experiments at wallops island, virginia to study lower ionosphere by direct local measurements and radio wave propagation
Radio frequency impedance probe measurements of ionospheric electron densities
Ionospheric electron density profiles obtained by the cw propagation technique and by rf impedance probe techniques
Rf impedance probe measurements of ionospheric electron density obtained by aerobee-hi rocket
Re-evaluation of ionospheric electron densities and collision frequencies derived from rocket measurements of refractive index and attenuation
Two rockets were flown to peak altitudes of 220 km in September 1959 to test various methods planned for future measurements of ionization parameters in the ionosphere, exosphere, and interplanetary plasma. The experiments used techniques which sample the ambient environment in the immediate vicinity of the research vehicle. Direct methods were chosen since indirect propagation techniques do not provide the temperatures of charged particles, are insensitive to ion densities, and cannot measure local electron densities under all conditions. Very encouraging results have been obtained from a preliminary analysis of data provided by one of the two flights. A new rf probe technique was successfully used to determine the electron density profile. This was indicated by its agreement with the results of a companion cw propagation experiment, particularly when the probe data were corrected for the effects of the ion sheath which surrounds the vehicle. The characteristics of this sheath were determined directly in flight by an electric field meter which provided the sheath field, and by a Langmuir probe which measured the total potential across the sheath. The electron temperatures deduced from the Langmuir probe data are greater than the neutral gas temperatures previously measured for the same location and season, but these measurements possibly were taken under different atmospheric conditions. Ion densities were calculated from the ion trap data for several altitudes ranging from 130 to 210 km and were found to be within 20 percent of the measured electron densities.