PDS_VERSION_ID = PDS3 RECORD_TYPE = STREAM OBJECT = INSTRUMENT INSTRUMENT_HOST_ID = LP INSTRUMENT_ID = MAGER OBJECT = INSTRUMENT_INFORMATION INSTRUMENT_NAME = "MAGNETOMETER - ELECTRON REFLECTOMETER" INSTRUMENT_TYPE = {"MAGNETOMETER", "ELECTRON REFLECTOMETER"} INSTRUMENT_DESC = " Instrument Overview =================== The Lunar Prospector Magnetometer and Electron Reflectometer (MAGER) instruments are based on the instruments flown on the Mars Global Surveyor spacecraft [ACUNAETAL1992]. Some changes were made to the Lunar Prospector versions to account for the spinning spacecraft. Also, there is only one magnetometer sensor on Lunar Prospector. The instrumentation consists of a 3-axis fluxgate magnetometer, a symmetric hemispherical electrostatic analyzer, and their common electronics box. The magnetometer (MAG) sensor is a wide-range (up to +/- 65,536 nT), low noise (6 pT RMS), high sensitivity (as low as +/- 2 pT), triaxial fluxgate magnetometer. The MAG sensor is an 11 x 6.5 x 9 cm box. The electron reflectometer (ER) has a 360 degree disk-shaped field-of-view. The electrostatic optics select energy and focus the particles onto an imaging detector. The ER sensor is a 12 cm diameter cylinder, 9 cm high. The combined mass of the Magnetometer and Electron Reflectometer is about 5 kg, and the two instruments use about 4.5 w of power. Science Objectives ================== The MAG/ER experiment will investigate the origin and nature of lunar crustal magnetic fields and constrain the size of a metallic core. The experiment will also provide global maps of the lunar crustal magnetic fields and provide estimates of the lunar induced magnetic dipole moment [BINDERETAL1998]. Platform Mounting Descriptions ============================== The MAG sensor is mounted at the end of the MAG/ER boom about 2.6 m away from the spacecraft bus. The ER and electronics box are mounted at the ends of a small cross bar, about 1 m inboard from the MAG. The ER unit is mounted so that its field-of-view includes the spin axis and is perpendicular to the boom. The only blockage of the ER field-of-view is the boom itself. Operational Considerations ========================== The MAG sensor uses a combination of thermal blanketing and heaters to maintain its operating temperature. The ER unit maintains its temperature using thermal blanketing, surface finishes, and its internal power dissipation. The magnetic fields measured by the MAG will be a combination of the Earth's magnetic field, the field carried from the Sun by the solar wind, and the Moon's field, which is extremely weak. The magnetic field at the lunar surface is also affected by local deposits of magnetic material. The ER can measure magnetic fields as weak as one-millionth of the strength of the Earth's magnetic field. Operation and Sampling Modes ============================ The magnetometer data are sampled 16 times a second, synchronous with the telemetry clock. Data are compressed by delta-modulation to 6-bits per axis per channel. Occasional full samples (12 bits per axis plus range) are collected. Principal Investigator ====================== The Co-I and magnetics group leader for the Lunar Prospector Magnetometer and Electron Reflector experiment is Dr. Robert Lin of the University of California, Berkeley. " END_OBJECT = INSTRUMENT_INFORMATION OBJECT = INSTRUMENT_REFERENCE_INFO REFERENCE_KEY_ID = "BINDERETAL1998" END_OBJECT = INSTRUMENT_REFERENCE_INFO OBJECT = INSTRUMENT_REFERENCE_INFO REFERENCE_KEY_ID = "ACUNAETAL1992" END_OBJECT = INSTRUMENT_REFERENCE_INFO OBJECT = INSTRUMENT_REFERENCE_INFO REFERENCE_KEY_ID = "CARLSONETAL1983" END_OBJECT = INSTRUMENT_REFERENCE_INFO END_OBJECT = INSTRUMENT END