How long would it take for a spacecraft with a mass of 30,000 kg, to go from LEO to reach and match the speed of a space station in geostationary orbit so it could dock with the station, using a Hohmann transfer orbit?
LEO speed 7.8 km/s, 160 km above the Earth GEO speed 3 km/s, height of 36,000 km ESA Space Transportation page
Thrust of the craft's engine 45 kN, modeled on the CSM. Wikipedia-Apollo CSM
Are there any other parameters I should include? If any of the information doesn't make sense please let me know.