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Development of a small satellite remote sensing payload for passive limb sounding of the atmospheric oxygen emission / Michael Deiml. Wuppertal, 2017
Content
Introduction
Background and Scientific Justification
The Mesosphere/ Lower Thermosphere (MLT)
Gravity Waves
Temperature Measurement Strategies for the MLT
Relevant Past, Current, and Future Remote Sensing Satellites
CubeSats and their Scientific Value
Scientific Objectives and Requirements of the Satellite Mission
AtmoCube-1 Mission Overview
Scientific Measurement
Measurement Geometry
Mission Design
The Precursor Mission
Measurement Simulation
Atmosphere Simulation
Observation
Instrument
Data Processing
Retrieval
Instrument Development
Instrument Design Parameter
Optical Design and Analysis
Structural Design
Thermal Design
Electrical Design
Characterization and Calibration
Pixel Response Non-Uniformity Correction
Dark Current Removal
Flat-Fielding
Phase Correction
Relative Calibration
Applied Post-Processing in this Work
Verification
Optical Bench Tests
Vibration Test
Thermal Vacuum Chamber Tests
Sounding Rocket Flight Campaign
Discussion
Summary and Future Applications
Literature
List of Figures
List of Tables
Appendix AtmoCube-1 Mission Overview
Electrical Power Subsystem
Communication and Power Distribution Architecture
Datarate and Communication Budget
Mass Budget
Technology Readiness Levels (TRLs) of Subsystems
Appendix Measurement Simulation
Oxygen Emission Model: Parameter and Errors
SHS Principles
Optimal SHS Parameter
Appendix Instrument Design
Instrument Design Parameter
Optical Bandpass Filter Properties
Grating Diffraction Equation
SHS Field-Widening Prism Angle Temperature Dependence
SHS Design
View Factor Calculation for Straylight Analysis
Appendix Verification
Images during YoYo-Despin
Images with View to Earth
Images with View to Space
Images of Atmospheric Limb