I looked in my Gurps Space Book under Reaction drives. With the moderate reaction installed in a 50 dton spaceship, you set aside space for 20 tons of liquid hydrogen to be used as reaction mass. The exhaust speed of the reaction drive is 18 miles per second which converts to 29 km per second. To generate 1/60-g of thrust, you need a moderate reaction engine that masses 5.416 tones and takes up 0.774 dtons costing $1,083,000. This spaceship can produce a total change in velocity of 14.8 km per second and can maintain this acceleration for a total of 25 hours to achieve this. This means an average velocity of 7.4 km per second. The orbital velocity of Earth is 29.79 by contrast, so starting with Earth's velocity, the spacecraft can impart an additional 7.4 km per second for 37.19 km/sec relative to the Sun. If the ship deploys a mag sail, it can cancel out the Sun's gravity and approach Mars at a velocity of 37.19 - orbital velocity of 24.13 km/sec for a relative velocity of 13.06 km/sec. At a minimum distance of 54,510,620 km, the space ship can get there in 48 days and then slow daown for an approach of 5.66 km/second after using its remaining reaction mass over a period of 12.5 hours to slow down, the remaining approach velocity can be bled off through atmospheric entry or areobraking in Mars' atmosphere. The ship then deploys parachutes to slow down further and applies landing rockets to make a soft touchdown on the Surface of Mars. To take off again, the ship would have to manufature more fuel and fly to the nearest Martian space elevator to take off.