ThrustTrust = T = [ (eta*P)^2 * 2 * pi *R^2 * rho ]^0.3333
T = thrust (in Newtons)
eta = prop hover efficiency = 0.7-0.8 is typical for unstalled low-pitch props
P = shaft power = voltage * current * motor efficiency (in Watts)
pi = 3.14159
R = prop radius (in meters)
rho = air density = 1.22 kg/m^3
There are exactly 2 things which effect thrust.
1)prop diameter is by far the most important. Thrust varies as the 4th power of the diameter. If you double the diameter of the prop (and the rpm stays the same) you will have 16 times the thrust.
2)RPM. Thrust varies as the 3rd power of RPM. If you double the RPM (and the diameter stays the same) you will have 8 times the thrust.