User contributions
25 January 2018
Deployment Mechanisms
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+9
Deployment Mechanisms
Created page with "== Trigger Mechanisms == === Pyrotechnic Cables and Bolt Cutters === frame|thumb This mechanism employs a small controlled expansion to propel a bolt toward..."
File:CoilableMast.png
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File:LazyTongs.png
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File:Telescopic.png
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File:FoldableMast.png
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File:Paraffin.jpg
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File:SMA2.jpg
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File:SMA1.jpg
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File:Burn1.jpg
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File:Pyro1.jpg
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Mechanical Subsystem
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-5
Mechanical Subsystem
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+35
Battery
Charge Current Rate
-4
Battery
Charging Voltage and Voltage Regulation
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Battery
Comparison between the batteries =
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Various Tests performed on Integrated Satellite
Random Loading
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Various Tests performed on Integrated Satellite
Created page with "Two models of satellite are made Qualification Model (QM) and Flight Model (FM). The QM is tested for larger range of loads as compared to the FM because for qualification you..."
File:Thermovac.png
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Mechanical Subsystem
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+55
Configuration Layout
Created page with "The satellite has many components ranging from a small sun sensor to larger solar panels. Everything needs to be placed on the structure of the satellite. Configuration Layout..."
File:ISSConfig.png
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Mechanical Subsystem
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+27
Transportation
Active vs Passive Vibration Isolation
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Transportation
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Transportation
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-2
Transportation
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+10,289
File:PvA.JPG
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File:HeatPipe2.png
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File:HeatPipe1.png
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File:Lovers.png
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File:Heater.png
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File:Radiator.png
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File:MLI.png
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File:Interferometer.png
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File:AVI.jpg
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File:Transmissibility.png
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File:PVI1.png
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Battery
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+20
Battery
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Battery
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Transportation
Created page with "Several mechanical and electrical aspects determine the transportation requirements needed for satellite. == Mechanical Factors =="
Mechanical Subsystem
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+4
Introduction to Mechanical Subsystem
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+85
Introduction to Mechanical Subsystem
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+6
Introduction to Mechanical Subsystem
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-9
Introduction to Mechanical Subsystem
Requirements on Structures
Introduction to Mechanical Subsystem
Created page with "The mechanical subsystem is responsible for designing and manufacturing the satellite structure while ensuring that the satellite can bear all the structural and thermal loads..."
Payload Subsystem
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+73
Attitude Determination and Control Subsystem
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-25