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Mars Atmosphere and Volatile EvolutioN (MAVEN) Mission. Particles and Fields Package Pre-Environmental Review May 22 -23, 2012 01 - Payload Science Overview D. L. Mitchell. MAVEN Science Questions.
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Mars Atmosphere and Volatile EvolutioN (MAVEN) Mission Particles and Fields Package Pre-Environmental Review May 22 -23, 2012 01 - Payload Science Overview D. L. Mitchell
MAVEN Science Questions MAVEN will determine the role that loss of volatiles to space has played through time, providing definitive answers about Mars climate history: • What is the current state of the upper atmosphere and what processes control it? • What is the escape rate at the present epoch and how does it relate to the controlling processes? • What has the total loss to space been through time?
MAVEN Top-Level Flowdown NGIMS IUVS LPW integrated analysis integrated analysis STATIC MAG, SWEA, SWIA, LPW SEP LPW - EUV
The PF Package Solar Wind Ion Analyzer (SWIA) – SSL Solar Wind Electron Analyzer (SWEA) – IRAP(CESR) / SSL Langmuir Probe and Waves (LPW) – LASP / SSL LPW/Extreme Ultra-Violet (LPW-EUV) – LASP Solar Energetic Particle Detector (SEP) – SSL Magnetometer (MAG) – GSFC Supra-Thermal and Thermal Ion Composition (STATIC) - SSL SWEA EUV LPW 2 PLCS SWIA SEP 2 PLCS MAG 2 PLCS STATIC
MAVEN Measures Drivers, Reservoirs, and Escape Rates SWEA SWEA SEP EUV NGIMS MAG MAG IUVS IUVS Neutral Processes Solar Inputs Plasma Processes LPW LPW SWIA SWIA STATIC
MAVEN Mission Architecture In situ and semi-global remote sensing measurements are made from the MAVEN elliptical orbit. Measurements are obtained down to the well-mixed lower atmosphere through five “deep dip” campaigns. Coverage of all local solar times and most latitudes, along with broad geographical coverage, results from precession of the MAVEN high-inclination orbit.
PF Instrument Operations S/C Attitude Inertial Point Inertial Point Sun-V Fly-Y slew slew slew slew APP Mode Sun-Nadir (STATIC priority) Sun-Nadir (STATIC priority) RAM-N RAM-H Fixed Fixed M M H L L LPW LPW-EUV Solar Monitor M M H L SEP L MAG H L L SWIA Solar Wind and Magnetosheath Modes (internally triggered) Iono Mode SWEA Solar Wind Mode Solar Wind Mode STATIC C C Pickup Ions & Magnetosheath RAM Pickup Ions & Magnetosheath 5600 6200 500 500 5600 Spacecraft Altitude (km) 0 45 90 135 180 225 270 Time Since Apoapsis (min) Key: H/M/L = high/medium/low data rates; C = ion conics and outflow Sun/Nadir Point Sun/Nadir Point
PF Measurement Requirements Program Level Requirements (MAVEN_PM_RQMT-0007) Mission Level Requirements (MAVEN_PM_RQMT-0005) PFP Functional Requirements (MAVEN_PFIS_RQMT-0016) Details for each instrument in backup slides. • In most cases, verification is based on calibration • Some verification procedures based on analysis (e.g., in-flight calibration) • Verification of PF measurement requirements is underway
Backup Slides Details of PF measurement requirements by instrument
STATIC Measurement Requirements STATIC measures low- and medium-energy ion composition, energy, and direction: Densities, velocities, and temperatures of suprathermal H+, O+, O2+, and CO2+ above the exobase with the ability to spatially resolve magnetic cusps Derived Level 3 measurement requirements:
SWEA Measurement Requirements SWEA measures properties of solar wind electrons that can drive escape: Energy distributions of solar wind, magnetosheath, and ionospheric electrons to determine the electron impact ionization rate, with an energy resolution sufficient to distinguish ionospheric photoelectrons from solar wind electrons Electron angular distributions to determine magnetic topology, with the ability to spatially resolve magnetic cusps. Derived Level 3 measurement requirements:
SWIA Measurement Requirements SWIA Measures properties of solar wind ions that can drive escape: Density and velocity distributions of solar wind and magnetosheath ions to determine the charge exchange rate and the bulk plasma flow from solar wind speeds down to stagnating magnetosheath speeds Derived Level 3 measurement requirements:
Cross Calibration of STATIC/SWEA/SWIA The angular and energy responses and the geometric factor (minus detection efficiency) for all three instruments are determined on the ground to within ~10% by calibrations and electrostatic optics simulations. Detection efficiency depends on MCP efficiency, which varies during the mission need a procedure to measure and track this efficiency for all three instruments.
Cross Calibration of STATIC/SWEA/SWIA Detection efficiency of STATIC determined by measuring START and STOP event ratios. (START with STOP)Validand (STOP with START)Valid STARTValidSTOPValid Consistency check: Measure total plasma density near periapsis and compare with calibrated LPW measurements. Absolute sensitivity of SWIA determined by cross calibration with STATIC in the outer sheath Absolute sensitivity of SWEA determined by cross calibration with SWIA and STATIC in the outer sheath and with SWIA in the solar wind. In-flight Calibration Plan: PF_SYS_35
SEP Measurement Requirements SEP Measures solar energetic particle input into upper atmosphere: Solar energetic particles that can interact with the upper atmosphere, with a time resolution sufficient to capture SEP events. Derived Level 3 measurement requirements:
MAG Measurement Requirements MAG measures solar-wind interactions and “mini-magnetospheres” Vector magnetic field in the unperturbed solar wind, magnetosheath, and crustal magnetospheres, with the ability to spatially resolve crustal magnetic cusps. Derived Level 3 measurement requirements:
LPW Measurement Requirements LPW shall measure electron temperature and number density measured in situ: Thermal electron density and temperature from the ionospheric main peak to the nominal ionopause with a vertical resolution of one O2+ scale height. LPW shall measure electric field wave power at frequencies important for ion heating. Derived Level 3 measurement requirements:
LPW/EUV Measurement Requirements EUV shall measure solar EUV input into upper atmosphere: Solar EUV irradiance at wavelengths important for ionization, dissociation, and heating of the upper atmosphere with a time resolution sufficient to capture solar flares. Derived Level 3 measurement requirements:
PF Measurement Resiliency If we lose any one instrument, do we lose any high-level objectives? (Y = Yes, S = Substantial, P = Partial, N = Not significant, - = Minimal contribution) PF