+We were totally stoked that the burn time matched simulation (once we factor
+in a tenth of a second or two before the motor came up to pressure!). We
+were also pleased that the max pressure was "right on time" at about 0.4
+seconds after coming up to pressure. The regressive curve seems a bit
+exagerated in the flight accel data, which seems completely explainable by
+the nozzle throat erosion causing pressure to faill during that period.
+
+Pretty cool for our first real flight test!