Abstract:Data from a VLF electric field antenna on board the spacecraft OV3‐3 show that the antenna response depends upon the local plasma density. Antenna impedances, calculated on the basis of a cold, magnetized plasma model and a warm, nonmagnetized, collisionless plasma sheath model, are compared with the data, showing that the sheath model is more appropriate. The response of the electric field antenna to constant onboard sources of electromagnetic interference is used with the antenna sheath impedance model to ca… Show more
“…A number of theoretical studies of radiation from a short dipole antenna surrounded by plasma have been carried out starting in the 1960s [e.g., Mlodnosky and Garriott , 1963; Balmain , 1964; Despain , 1966]. The subject was extensively studied in the 1970s [e.g., Koons et al , 1970; Shkarofsky , 1972; Kuehl , 1974; Laframboise et al , 1975; Adachi et al , 1977], and work continued later on until recently [e.g., James , 2000; Nikitin and Swenson , 2001; James , 2003]. While these works have brought a conceptual understanding of the antenna‐plasma interaction, some models often lacked self‐consistency, since in most cases electrostatic conditions were assumed and the radiation resistance was not considered in the system.…”
Section: Introductionmentioning
confidence: 99%
“…Experimental investigations, however, were rare and were mainly made at the ionospheric heights. They were carried out on board the OV3‐3 spacecraft [e.g., Koons et al , 1970], ISIS satellite [ James , 1980], and also rockets [ Chugunov et al , 2003; James , 2003]. In most cases, the measured voltage or antenna potential as function of operating frequency was compared to those calculated using impedance theories for dipole antenna in plasma.…”
Section: Introductionmentioning
confidence: 99%
“…In most cases, the measured voltage or antenna potential as function of operating frequency was compared to those calculated using impedance theories for dipole antenna in plasma. It has been demonstrated that an agreement between the observations and theory was reasonably good when the sheath effect is taken into account [e.g., Koons et al , 1970; James , 1980] and that the propagation near the resonance cone requires special treatment [ Chugunov et al , 2003]. Song et al [2007] reported some preliminary experimental results obtained with the RPI‐IMAGE instrument and compared the measurements with their sheath model.…”
[1] We use the radio plasma imager (RPI) on the IMAGE satellite to investigate the impedance characteristics of an active electric antenna in space plasma at whistler mode frequencies. A dedicated experiment was carried out on 21-22 September 2005 for two orbits in the plasmasphere. The input impedance characteristics of the dipole antenna submerged in plasma is determined at whistler frequencies. The results are consistent with a physical model in which the antenna is negatively charged to a large voltage and the plasma around each antenna element forms an ion sheath that varies with time in its radius. Within the plasmasphere, these sheaths are a part of the antenna-plasma system and represent a capacitive component of the tuned antenna circuit. It is shown that, inside the plasmasphere, the RPI antenna capacitance varied from 430 to 480 pF. The plasma sheath formed around the antenna in the plasmasphere increases its capacitance by 20%-30% with respect to the near-free space capacitance (364 pF). Comparison of these values to model calculations shows good agreement with a difference smaller than 5%. Measurements of the antenna input resistance showed that, inside the plasmasphere, its value was between 200 and 500 W, varying considerably with changes in the ambient electron density and cyclotron frequency. The measured antenna input resistance is compared to model calculations.
“…A number of theoretical studies of radiation from a short dipole antenna surrounded by plasma have been carried out starting in the 1960s [e.g., Mlodnosky and Garriott , 1963; Balmain , 1964; Despain , 1966]. The subject was extensively studied in the 1970s [e.g., Koons et al , 1970; Shkarofsky , 1972; Kuehl , 1974; Laframboise et al , 1975; Adachi et al , 1977], and work continued later on until recently [e.g., James , 2000; Nikitin and Swenson , 2001; James , 2003]. While these works have brought a conceptual understanding of the antenna‐plasma interaction, some models often lacked self‐consistency, since in most cases electrostatic conditions were assumed and the radiation resistance was not considered in the system.…”
Section: Introductionmentioning
confidence: 99%
“…Experimental investigations, however, were rare and were mainly made at the ionospheric heights. They were carried out on board the OV3‐3 spacecraft [e.g., Koons et al , 1970], ISIS satellite [ James , 1980], and also rockets [ Chugunov et al , 2003; James , 2003]. In most cases, the measured voltage or antenna potential as function of operating frequency was compared to those calculated using impedance theories for dipole antenna in plasma.…”
Section: Introductionmentioning
confidence: 99%
“…In most cases, the measured voltage or antenna potential as function of operating frequency was compared to those calculated using impedance theories for dipole antenna in plasma. It has been demonstrated that an agreement between the observations and theory was reasonably good when the sheath effect is taken into account [e.g., Koons et al , 1970; James , 1980] and that the propagation near the resonance cone requires special treatment [ Chugunov et al , 2003]. Song et al [2007] reported some preliminary experimental results obtained with the RPI‐IMAGE instrument and compared the measurements with their sheath model.…”
[1] We use the radio plasma imager (RPI) on the IMAGE satellite to investigate the impedance characteristics of an active electric antenna in space plasma at whistler mode frequencies. A dedicated experiment was carried out on 21-22 September 2005 for two orbits in the plasmasphere. The input impedance characteristics of the dipole antenna submerged in plasma is determined at whistler frequencies. The results are consistent with a physical model in which the antenna is negatively charged to a large voltage and the plasma around each antenna element forms an ion sheath that varies with time in its radius. Within the plasmasphere, these sheaths are a part of the antenna-plasma system and represent a capacitive component of the tuned antenna circuit. It is shown that, inside the plasmasphere, the RPI antenna capacitance varied from 430 to 480 pF. The plasma sheath formed around the antenna in the plasmasphere increases its capacitance by 20%-30% with respect to the near-free space capacitance (364 pF). Comparison of these values to model calculations shows good agreement with a difference smaller than 5%. Measurements of the antenna input resistance showed that, inside the plasmasphere, its value was between 200 and 500 W, varying considerably with changes in the ambient electron density and cyclotron frequency. The measured antenna input resistance is compared to model calculations.
“…According to the theory of Cornwall et al [1971], ring current energy is dissipated at the plasmapause. If we assume that the arc is generated as a consequence of dissipation of ring current energy [Cole, 1965] The VLF method that 0V3-3 (1966-70A) used to measure the location of the plasmapause has been described by Koons et al [1970]. According to their results the plasmapause was located at L --2.5-2.9 at 0213 LT, 0036 UT on December 16, 1966.…”
Three midlatitude red arcs were measured by the night airglow photometer on board OV1‐10 (1966–111B) during the winter of 1966–1967. One arc was observed as a conjugate phenomenon. Another arc was observed for 2 days at a constant local time and was found to decrease in intensity, increase in width, and move to higher L values with universal time. Both arcs were found to be associated with the plasmapause, the location of which was determined from the VLF measurements made by OV3–3 (1966–70A). These observations are shown to be consistent with the theory that SAR arcs are generated at the plasmapause as a consequence of the turbulent dissipation of ring current energy.
“…The data are from the 712-keV electron channel of the OV3-3 (1966-70A) magnetic spectrometer and the 400-Hz frequency band from the electric field antenna on the same satellite. (See Vampola [1969] and Koons et al [1970] for instrumentation details. The geometric factors listed by Vampola [1969] are all a factor of 4 too high owing to an error in the original calculations.)…”
By using simultaneous observations of low‐altitude energetic electron fluxes from the magnetic electron spectrometer on OV3‐3 and equatorial electron fluxes observed by ATS 1 a previously identified strong pitch angle scattering mechanism is shown to be a low‐altitude phenomenon only. The relationship between this scattering process and the apparent location of the outer‐zone energetic electron boundary as observed by low‐altitude polar‐orbiting satellites is demonstrated. The process explains observations of rapid electron boundary motions during geomagnetically quiet times. In addition, by assuming that the process also explains the energetic electron spike sometimes seen at the apparent outer‐zone cutoff the magnitude of the spike itself is used to determine the high‐altitude limit of the rapid‐scattering region.
scite is a Brooklyn-based organization that helps researchers better discover and understand research articles through Smart Citations–citations that display the context of the citation and describe whether the article provides supporting or contrasting evidence. scite is used by students and researchers from around the world and is funded in part by the National Science Foundation and the National Institute on Drug Abuse of the National Institutes of Health.