Guys, you’re making it all too hard. Just ask the resident rocket scientist. 
(Okay, so my title is aerospace engineer, not rocket scientist…but who’s gonna argue?)
The equations for thrust is net momentum flux (mass flow rate times velocity) plus the force of the pressure differential (difference between exit and freestream pressurs times exit area)
Here, mass flow rate (m is the closest I could come to "m dot," which is dm/dt) is how much mass leaves the urethra every second. Normally, m
= p · V · A, but in this case, it’s easier to calculate by dividing mass expelled by time it takes to do so. so m` = (total mass of urine)/(time of urination)
T = (m V)[sub]e[/sub] - (m
V)[sub]0[/sub] + (p[sub]e[/sub] - p[sub]0[/sub]) · A[sub]e[/sub]
Now, the freestream momentum is effectively zero, since the fluid velocity in the bladder is negligible. The pressure difference across the urethral opening is very small, and acts over a miniscule area, so the last term can also be ignored. This reduces our thrust equation to:
T = m` V
(simple, huh?)
Using the numbers from astro’s page about urination, we can calculate mass flow rate and velocity. m = 1 lb[sub]m[/sub] / 10 sec = 0.00311 slug/s. And from my above equation, V = m
/(p · A)
m` = (0.00311 slug/s)
p = water = 1.94 slug/ft[sup]3[/sup]
A = area of 5-mm diameter circle = pi · (0.0082021 ft)[sup]2[/sup] = 2.113×10[sup]-4[/sup] ft[sup]2[/sup]
V = (0.00311)/(1.94 · 2.113×10[sup]-4[/sup]) = 7.585 ft/s
so T = m`· V = (0.00311 slug/s)(7.585 ft/s) = 0.0236 lb (or 0.67 g)
It’s a rough order of magnitude apprximation to be sure…but there you go.
(About halfway throguh this calculation, I was reminded why I hate British units. Slugs…what? But the soda bottle numbers were given in oz, so I had to convert something. I obviously chose wrong. Kill me now.
)