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Updates to the avionics sled to improve ease-of-use during launch. |
The avionics sled fits into the avionics bay tube of the rocket. The sled must hold two altimeters and two 9V batteries. On the day of launch, altimeters need to be wired twice - first for ground test and then for the main flight. In order to be time-efficient, it is important that the altimeters can be easily accessed.
The AirBears avionics sled was the same as that used for Arktos. It fit into a 4" rocket and was used for the test launch on Nov 16, 2019. Overall, the design was effective as all components were housed and both parachutes successfully deployed. However, there was difficulty in wiring the altimeters due to their placement along the raised edges where the sled slides into the avionics bay.
The goals of the redesign of the avionics sled for the IREC 2020 rocket were the following:
- Optimize the avionics bay for a 6" rocket
- Address wiring concerns from AirBears to improve ease-of-use during launch
The new chosen design was an I-beam model, in which the batteries were placed in a center section of the sled and one altimeter was mounted to each side, as shown below. This design somewhat improved the space usage in the vertical direction, but there was significant unused horizontal space. The Recovery subteam selected this design because they felt it was more important to be able to wire the altimeters efficiently at launch than to use the least possible space.
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The goals for the avionics bay designs for the 2022 Stage Separation vehicle were as follows:
- Integrate sufficient room in at least one avionics bay to accommodate the Common Avionics Stack (CAS).
- Integrate sufficient room to accommodate off-the-shelf altimeters in addition to CAS, to allow for flights without CAS integration and also ensure failsafes for early CAS test launches.
- Include multiple avionics bays, as the two-stage nature of the SSEP vehicle requires at least one for each stage.
In the end, the SSEP vehicle incorporated three different avionics bay designs:
- An upper stage avionics sled used to manage recovery of the upper stage. Its overall structure similar to the IREC 2020 design, but with an additional hole to accommodate CAS. This design placed CAS in its own "hole" in the bottom while the altimeters and batteries were secured to a central "wall".
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- An interstage avionics bay used to ignite the upper stage motor after stage separation. Its structure is different compared to the other ones; because of the limited space available in the interstage, it is not CAS-compatible. It has similar top and bottom pieces that neatly slide into each other, and are held closed by the bulkheads and spacers.
- A lower stage avionics bay used to manage recovery of the lower stage. It is somewhat different from the IREC 2020 design but maintains the same basic structure, with a sled sliding out of two rings, which in this case are connected with an overall housing. Similar to the upper stage avionics bay, it places CAS in its own "level" while the other altimeters are kept on the second level.
