jupiter ganymede orbiter medium frequency receiver and other contributions

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Jupiter Ganymede Orbiter Medium Frequency Receiver and other contributions W. Kurth & D. Kirchner The University of Iowa 11 Jan. 2011

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Jupiter Ganymede Orbiter Medium Frequency Receiver and other contributions. W. Kurth & D. Kirchner The University of Iowa 11 Jan. 2011. RPWI Block Diagram. Medium Frequency Receiver. MF Receiver Description. 3-channel receiver 1 kHz – 1 MHz bandpass (could be modified, within reason) - PowerPoint PPT Presentation

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Page 1: Jupiter Ganymede Orbiter Medium Frequency Receiver and other contributions

Jupiter Ganymede OrbiterMedium Frequency Receiver and other

contributions

W. Kurth & D. KirchnerThe University of Iowa

11 Jan. 2011

Page 2: Jupiter Ganymede Orbiter Medium Frequency Receiver and other contributions

RPWI Block Diagram

Page 3: Jupiter Ganymede Orbiter Medium Frequency Receiver and other contributions

Medium Frequency Receiver

Page 4: Jupiter Ganymede Orbiter Medium Frequency Receiver and other contributions

MF Receiver Description• 3-channel receiver• 1 kHz – 1 MHz bandpass (could be modified, within reason)• Prime channel is SSR antenna, other two are LP differential inputs,

sensors 1,3 and 2,4• Designed to simultaneously capture waveforms from all 3 channels,

but could choose n of 3.• Uses 14-b A/D converters sampling at 2.5 MHz (driven by upper

frequency limit)• Anticipated operation would be to capture 2N (e.g. 1024, 4096…)

samples and perform DSP in the CDPU once per m seconds• Results in high instantaneous rate to CDPU but with low duty cycle so

that telemetry from RPWI for this receiver can be arbitrarily small.• Based on Juno, RBSP heritage, TRL 8

Page 5: Jupiter Ganymede Orbiter Medium Frequency Receiver and other contributions

MF Receiver Options• Original concept was to pass digital waveforms off to the RPWI DSP

for processing.• Given discussion of yesterday, we’ve briefly discussed adding a

Juno-like FPGA to the MF receiver board which would compute spectra and then pass the (greatly) reduced data set off to the DPU.– Would need some basic services

• Load s/w into FPGA• Supply clock for A/Ds and FPGA• Issue start signals to the FPGA to initiate data capture and processing• Some interrupt servicing

– Could FFT two channels simultaneously; third channel would have to be done with second FFT process.

– Would still want the ability to move compressed (~3:1) waveforms to DPU to allow brief snapshots of high resolution waveforms (ala Cassini and others); these data can be buffered in the MFR for some time.

Page 6: Jupiter Ganymede Orbiter Medium Frequency Receiver and other contributions
Page 7: Jupiter Ganymede Orbiter Medium Frequency Receiver and other contributions
Page 8: Jupiter Ganymede Orbiter Medium Frequency Receiver and other contributions

Digital Electronics Subsystem Transmitter Assembly

RX Isolation

Notional Radar Block Diagram

TX

LF Power Amplifier

HF Power Amplifier

RX Isolation

LFMatching Network

HFMatching Network

ADC

LFReceiver

HFReceiver

ADC

Radio Plasma Wave Receiver

RF receiver Assembly

Switch

Antenna

Page 9: Jupiter Ganymede Orbiter Medium Frequency Receiver and other contributions

Sharing of SSR Antenna• SSR instrument should have priority in the use of the

antenna• The risk of failure in the devices (e.g. switches) used to

connect the antenna to RPWI should be minimized and in any case the adopted solution should guarantee that in case of failure the antenna remains connected with the SSR instrument

• The two instruments should be protected each other from hazardous electrical effects

• The RPWI instrument will use the antenna only for receiving signals (no active transmission mode will be possible)

Page 10: Jupiter Ganymede Orbiter Medium Frequency Receiver and other contributions

Backup – Some Science

Page 11: Jupiter Ganymede Orbiter Medium Frequency Receiver and other contributions

EJSM Synergistic Science• All points are designed to illustrate the value of passive radio

and plasma wave measurements on both JEO and JGO– Satellite-magnetosphere interactions

• Io• Ganymede• Europa

– Synergistic two-point measurements in the magnetosphere• Galileo-Cassini example

– Thermal plasma measurements• Passive wave measurements can provide among the most accurate plasma

density measurements

– Support for subsurface sounding• Monitor Jovian radio emission activity• In situ plasma density

– Other measurements of interest• Dust flux and size distribution• Lightning detection

Page 12: Jupiter Ganymede Orbiter Medium Frequency Receiver and other contributions

Satellite Interactions• Galileo plasma wave observations led to discovery of Ganymede’s magnetosphere• Identification of upper hybrid resonance band provides plasma density• Galilean satellites all show strong interactions with Jupiter’s magnetosphere• Plasma wave spectrum provides evidence of wave-particle interactions and the flow of mass and energy resulting from the magnetospheric interaction.

Page 13: Jupiter Ganymede Orbiter Medium Frequency Receiver and other contributions

Synergistic Two-Point Measurements• Galileo – Cassini radio and plasma wave measurements revealed the response of the Jovian magnetosphere to variations in the solar wind.• Two-point measurements can help distinguish between global magnetospheric dynamics and spatial variations.• Approach solar wind observations provide valuable solar wind input for comparison with magnetospheric observations.• Magnetospheric observations by one spacecraft provides a baseline for other spacecraft in orbit (or flying by) a Galilean satellite.• Jovian radio emission monitoring provides a measure of magnetospheric activity for other spacecraft orbiting (or flying by) a Galilean satellite.

Page 14: Jupiter Ganymede Orbiter Medium Frequency Receiver and other contributions

Thermal Plasma Measurements• A plasma wave instrument provides accurate plasma density measurements, a fundamental parameter of the Jovian environment and essential to many modeling efforts.• Identification of various resonances

(upper hybrid) or cutoffs (electron plasma frequency, L=0, or R-X cutoff frequencies.

• Quasi-thermal noise spectroscopy• Invaluable for calibration of plasma instruments.

Page 15: Jupiter Ganymede Orbiter Medium Frequency Receiver and other contributions

Maximum Ionospheric Densities and Plasma Frequencies

• Callisto1 17,400 cm-3 1.2 MHz

• Ganymede2 400 cm-3 180 kHz• Europa3 9,000 cm-3 900

kHz• Io4 277,000 cm-3 4.7

MHz1Kliore et al., JGR, 2002.2Eviatar et al., PSS, 2001.3Kliore et al., Science, 1997.4Hinson et al., JGR, 1998.

Support for Subsurface Radar Sounders• Provides monitor for Jovian radio emission activity at sounder frequencies• Provides measurement of local plasma densities (plasma frequencies) in vicinity of Galilean satellites. Some of these are close to possible sounding frequencies.

Page 16: Jupiter Ganymede Orbiter Medium Frequency Receiver and other contributions

Other Measurements Possible with a Plasma Wave Instrument• Detection of lightning-generated whistlers provides evidence of atmospheric lightning.• Micron-sized dust impacting the spacecraft at several km/sec creates an impulse in a plasma wave receiver that allows an estimate of the dust flux as well as the size distribution.

Page 17: Jupiter Ganymede Orbiter Medium Frequency Receiver and other contributions

Summary• Passive radio and plasma wave measurements made on both

JGO and JEO provide support for subsurface radar sounding investigations.

• Additionally, these measurements address a wide range of objectives central to EJSM science.

• The ability to make two-point measurements in and near Jupiter’s magnetosphere enable a number of new types of advances.

• The existence of a ‘long’ dipole antenna makes the addition of a radio and plasma wave receiver substantially easier to accommodate.

• Passive radio and plasma wave measurements can be scheduled so as to be complementary to the SSR observations.