Here's the detail of the beams..
Sorry was busy yesterday, now I have a little time to review again.
In terms of the beams
per se, i couldn't get exactly the same values you posted, in terms of deflection, from the data you supplied. Thus the data is slightly incorrect, but "consistent".
A dwg/diagram of exactly how/where you loaded this is soooooooooooooooooo much easier, avoids misunderstanding and confusion.
So, if i take "mid values" since i can interpret you "words" into actual locations of loads, (applied loads and locations), several ways, since the values are also inconsistent, however, I get "similar" values, that being a deflection of 65mm, or 2.5" in your funny units.
The thing to note is that the stress in the beam is roughly a FoS of just 2 in compression.
It appears from your beam that the only thing separating the two 7/8 x 2.1/4 sections are the spacers which are glued to the 96" lengths?? Therefore the shear strength of your beam is the strength of the epoxy glue in shear. Which is similar (relatively, but actually not very good) but less than that of the compression strength of the
Juniper. Thus the beam shall fail in shear first. So what shear loads will the beam experience? See below.
Depending upon the values I use, to get my answers, the shear stress in the epoxy glue is approaching the failure of typical
epoxy.
However, all this is moot. Since what loads will you outriggers experience?...you need to define the loads then see if the beams are suitable.
BTW..flexibility in structure, can, if designed correctly, be a good thing. However it can also be a disaster in the wrong applications. You don't want your outriggers moving independently from the main hull!