Magnetometers for space measurements over a wide range of field intensities
Fluxgate and Ru vapor magnetometers for space measurements over wide field intensities, reducing electronic phase shift and experiment weight
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Fluxgate and Ru vapor magnetometers for space measurements over wide field intensities, reducing electronic phase shift and experiment weight
ALSEP magnetometer mission and environmental requirements and mechanical design
Active RC bandpass filter for space fluxgate magnetometer, using state variable synthesis
Proton magnetometer measurements from satellite Cosmos 49, observing residual and broad magnetic anomalies
Lunar surface local magnetic field measurement, describing Apollo 12 magnetometer
Development of wide range linear fluxgate magnetometer
ATS 5 ground station magnetometer data processing program
Design and development of optically pumped resonance magnetometer for determining vectoral components in spatial coordinate system
Image effects and vibrating sample magnetometer
Determination of lunar electrical conductivity profile from joint power spectral density analysis of data from Apollo 12 and Explorer 35 magnetometer data
Fluxgate magnetometer for measuring magnetic field along two axes using one sensor
Lunar portable magnetometer experiment to measure steady magnetic field at different sites in Fra Mauro region - Apollo 14 flight
Simultaneous two magnetometer measurements of weak magnetic fields in interplanetary space, near moon and planets by satellites in presence of spacecraft field
Lunar electrical conductivity profile from joint power spectral density analysis of Apollo 12 and Explorer 35 magnetometer data
Sensitive magnetometer capable of measuring field strengths of 10 nanogauss is described. High permeability core is aligned parallel to magnetic field in first stage. In second stage, ferromagnetic toroid saturates rapidly. Adjustment of turns and area ratios of each stage provides wide range of sensitivities.
A tri-axis flux-gate magnetometer was used on four Gemini spacecraft for determination of the magnitude and direction of the local geomagnetic field with respect to the spacecraft. Conclusions derived from the data are not only important to the proton-electron spectrometer experiment, but also are of significance to any directional charged particle experiments that may be conducted. Even though the Gemini spacecraft was not clean magnetically, the data could be reduced to a form that supplied directional information on the magnetic field in relation to the spacecraft. Stray fields were the result of spacecraft structure, not the result of current flows that were produced within the spacecraft electrical systems. Efforts were made to reduce spacecraft stray fields and to facilitate the acquisition of more accurate data.
A number of conductivity models were investigated for compatibility with Apollo 12 magnetometer data. Except at the highest frequencies, a simple core-crust model is compatible with the observed dayside transfer function, which is expressed as the ratio of the lunar surface field spectrum to the interplanetary magnetic field spectrum. All conductivity profiles exhibit a peak near 1500 km, when the models are constrained to conform to the observed flat response at the higher frequencies. However, at frequencies above .01 Hz the long wavelength limitation of the theoretical model is no longer valid. A plausible explanation for the difference between the north-south and east-west transfer functions is that it is due to a time-varying compression of the remanent (dc) field at the Apollo 12 site by fluctuations in the solar wind plasma.