Moment of Inertia for connected, hinged panels

AI Thread Summary
The discussion focuses on calculating the moment of inertia (MOI) for a solar panel array consisting of three connected panels on a spacecraft. Each panel measures 0.2 meters by 0.3 meters and is hinged along the 0.3-meter side. The user is unsure about their approach to calculating the MOI, given that the panels will be released simultaneously from a folded position. The deployment mechanism is crucial for determining the correct calculation method, as the panels will move together when released. Clarification on the motion control and a visual aid were suggested to assist in understanding the problem better.
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Homework Statement


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There is a solar panel array of 3 panels connected to a spacecraft . The panels in the array are connected linearly (in a row: panel1 + panel2 + panel3 + spacecraft ) with hinges. They are all 0.2 meters by 0.3 meters and connected along the 0.3 meter side using 2 hinges for each panel. I'm looking for the MOI so that I can calculate the angular momentum of all 3 panels when they are released from their folded position once the craft is in orbit. They are folded together on the hinged sides and all 3 are in a "pile" before being released.

Homework Equations

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I=1/3*M*a^2 'a' being the length of the shorter side in this case 0.2

The Attempt at a Solution


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Innermost panel has to swing outward with the mass of the other 2 attached to it: I=1/3*(M*3)*a^2
Middle panel has to swing outward with the mass of itself plus outer panel attached to it:
I = 1/3*(M*2)*a^2
outermost panel: I = 1/3*M*a^2

Since the panels are connected and moving simultaneously when released, I'm not sure this is the way to do this and I can't find any similar examples which makes me think I'm really missing something.
Any help would be greatly appreciated!
 
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I doubt I will be able to help but I think sketch might help. Are the panel's "rolled" or "consterina" pattern?
 
Answer you are looking for depends on how the motion of the panels is being controlled . You really need to know how the deployment mechanism works .
 
CWatters said:
I doubt I will be able to help but I think sketch might help. Are the panel's "rolled" or "consterina" pattern?
Concertina pattern.
 
Nidum said:
Answer you are looking for depends on how the motion of the panels is being controlled . You really need to know how the deployment mechanism works .
The panels will be released all at once - a chord holding them "pinned down" in their folded position will break and the entire solar panel array comes free at once.
 
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