The structural modules for the assembly of Iris is built using a single common component that will be manufactured in a batch, and then is modified slightly for the specific needs of each subsystem. The general dimensions for these 1/2 U shells is given in the following drawings:
Note that Power Submodule currently has a NX software bug preventing the creation of new drawings.
The Power Module for the MB-SAT uses two half shells and has a prescribed working volume laid out by the following drawing:
The small cut through the entire working volume allows for a pass-through for cables from the interface board in the Power module up into to the ADCS module. The second "chunk" that has been removed from the Power Module allows for one of the Torque rods to extend slightly into the Power Module.Â
In addition to the ICD, the parts and layout of the module has also been created.
The Power Module for the MB-SAT uses two half shells and has a prescribed assembly laid out by the following drawing:
Due to the planned method of adding the batteries to the Power Module, the Power Control Unit board (PCU) has an additional set of restrictions on its Printed Wiring Board (PWB) maximum dimensions. The following layout shows the PCU dimensions:
The Batteries will be mounted directly to an aluminum milled part referred to as the "battery saddle."
The final major component for the PWR module is the shell modules. The structural components use two of the 1/2U shells defined above, with one of them modified to accommodate the pass through for the Z torque rod. The dimensions for that cut are shown here.
The final major component for the PWR module is the shell modules. The structural components use two of the 1/2U shells defined above, with one of them modified to accommodate the pass through for the Z torque rod. The dimensions for that cut are shown here.
Two Separation switch assemblies are used in the lower half U-shell of the power model. the separation switches contain 3 electrical switches that determine whether the pins are still compressed in the Nanoracks deployer. The 4 pins collectively provide 9N of force.Â
A single RBF pin is used to compress an electrical switch to ensure the system is off until placed in the Nanoracks container. Prior to launch the pin shall be removed.
The ADCS Module for the MB-SAT uses one half shell and has a prescribed working volume laid out by the following drawing:
As with the Power module, the small cut through the entire working volume allows for a pass-through for connections from the Power module up through ADCS and into the Payload Module.Â
The second "chunk" that has been removed from the ADCS working volumes are for the torque rods. these torque rods will be mounted directly to the board.
The internals for the ADCS module are shown in the following assembly drawing.
As can be seen from this drawing the torque rods will be mounted directly to the ADCS control board itself. By mounting the rods in this way the assembly of the module will be easier for final implementation as they can be assembled outside the module and connected to the board allowing for more access to electrically connect the wires from the torque rods to the board. However, in doing so, there are additional restrictions added to the ADCS board, with regards to the maximum height that components can be (3mm).
A major component for the ADCS module is the shell module. The structural components uses one 1/2U shells defined above, modified to accommodate the Z torque rod. The dimensions are shown here.
The COMS Module also houses the CDH board and has a working volume as follows:
While the COMS module is made from the 1/2U shell, the height of the module is noticably less than that of the ADCS module. The additional space has been reserved for the Antennas and deployment systems.Â
COMS, CDH and the Antenna/deployment system are assembled into the module as shown.
The following edits are made to a 1/2U Shell to accommodate the COMS module.Â
Both the CDH and COMS interface boards have the same surface areas. CDH has a more restricted height on components, however the CDH components do not have significant heights that are cause for concern with the height restriction. The COMS CCA is allowed a greater height for the transceivers. Â
The additional 5.5 mm limit around the corner and center mounting points, ensures that no components will be placed where the mounting standoffs or bolt heads will be for the mounting hardware for the two boards.
In order for the Solar Panel Deployment System to fit within the deployer it has the maximum working volume defined below: