SODA Features
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Spacecraft Geometry Builder Used for Plume Impingement Analysis - Using Rectangles
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6DOF Thruster Jet Select Algorithm - Using Rectangles
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Thruster Tables and Duty Cycles - User Can Specify
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Multiple Spacecraft Library - DSG, ISS, Progress, Soyuz, MARE (Lander)
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Prox-Ops Model - Specifiable Standoff Distance
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Vecor Plume Model - Includes Thrust Decay Model
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Plume Induced Disturbance Calculation - Torque, Momentum, Propellant, Free-Drift Rates

SODA Analysis Capabilities
Spacecraft/Visiting Vehicles
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Calculate Translational and Rotational Jet Select
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Calculate Translational & Rotational Control Authority
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Evaluate Impact of Different Thruster Duty Cycles
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Monte Carlo Analysis for Delta CM Impact on Jet Select & Control Authority
Stations
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Calculate Plume Impingement Induced Disturbances
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Monte Carlo Analysis for Parameter Impact on Plume Impingement - Delta CM, Delta Orientation, VV Standoff
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Evaluate and Design Performance During VV Prox-Ops
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Perform Capabilities Listed Under Spacecraft/Visiting Vehicles