This is a short overview of the front end and readout electronics of the FGT. The emphasis is on providing some documentation on all the components. At present most of the items exist only as prototypes, I will try to keep this page current as things get finalized.
First, the front end board, which has 5 APV chips. Two front end boards are used per FGT quadrant (24 quadrants total). One sits at each end of the quadrant. As four quadrants fit together to form an FGT disk, the pairs of front end boards from adjacent quadrants physically sit close to each other. They are serviced by a common cable, interconnect board, and terminator board (to be described shortly).
Below is a picture of the first FGT quadrant (actually just a mechanical test assembly, the pad plane is an old design and is defective). Apologies this is a shiny object photographed on a shiny table in the Bates cleanroom. What you see here is mainly the aluminized mylar gas window which is also the ground plane, sits a couple of mm above the pad plane. On each end of the quadrant is a row of five Samtec MEC6 card-edge connectors (0.635 mm contact pitch): four 140 pin connectors and one 80 pin in the center of the other four. This connects the 640 = 5 APV * (128 ch/APV) signals from the pad plane to the FEE board. The ground is carried separately (see description below). The constraints on FGT inner and outer radius do not permit assigning any of these connector contacts to grounds.
Below is a picture of a front end board installed on an FGT quadrant. This is a view from "outside" i.e. this is the side of the front end board that does not have the APV chips. Actually in this picture is a mechanical mockup board, but is mechanically identical to the final design. The white RTV which can be seen in this picture is covering the edge of this quadrant assembly.
And here is the actual front end board. In this and the picture above you can see the two ground contact points which will be fastened with screws and washers to wide contact strips extending from the ground foil. This provides the connection of APV signal ground. The ground foil is also similarly connected to the bypass capacitor feeding bias voltage to the bottom of the last GEM foil (connections not detailed here).
Note that it is the back side of this board that would be seen in the quadrant picture above. The two front end boards serviced as a pair have the APV chips mounted on the outward facing sides. Similarly the ground foil connections are made on this outward facing side. From the quadrant's perspective, the chip side of the APV board faces in toward the center of the quadrant.
The front-end board is serviced by the "interconnect board" on one end and a "terminator board" on the other. All interface lines run through from end to end so that the design is symmetrical. Half of the frontend boards have the terminator on the right in this picture, half have the interconnect board on the right. There is only a single flavor of front end board.
The schematic of the front end board is (here). It consist only of five APV chips and a minimal set of support components.
The APV chip is a 128-channel preamp / shaper / SCA / readout mux chip developed for CMS tracker silicon, and also subsequently deployed for GEM readout in COMPASS. Most of the operational details are described in the user guide and in presentations available on the CMS tracker web pages. The APV chip incorporates an analog FIR filter (what the user guide refers to as deconvolution mode) for tail cancellation / pileup reduction at the expense of higher noise. We don't intend to make use of it. It should be noted that the appropriateness of the (fixed) filter coefficients is of course dependent on the sample clock rate. Which is another reason we don't intend to use it.
The APV chip sample clock can be run at least as fast as 40 MHz (as in CMS). For RHIC, we prefer to lock to a multiple of our collision frequency so that the signals can be synchronously sampled avoiding any additional complications or errors from asynchronous sampling. We will use 4x RHIC strobe, 37.532 MHz, a reasonable match to the capability of the APV chip.
The APV chip readout clock can be the sample clock or 1/2 the sample clock rate. With 1/2 the sample clock a single-point readout requires 280/37.532 MHz = 7.46 us. This is amply fast in comparison with other STAR detectors even if multi-point readout is employed. So we will use only the 1/2 rate readout because it significantly eases the signal transport problem.
[Insert here description of the interconnect board / terminator board. (voltage reg, clk/trig receiver, temp sensors, POR circuit, terminations)]
The above comprises the front end electronics subsystem. The interfaces from the front end electronics to the readout electronics are, in total:
(more description/documentation of the readout system to come...)