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What is the definition and difference between conjunction-class and opposition-class Mars missions according to the source?

 title: 'Figure 11—The 1967 Planetary Joint Action Group's Mars flyby spacecraft releases automated probes and deploys instruments. Close Mars flyby would last mere hours, but the astronauts would study themselves throughout the mission, helping to pave the way for future Mars landing expeditions. (NASA Photo S-67-5999)'

In the source, a conjunction-class Mars mission is one that uses low-energy transfers to Mars and back, with a long stay at Mars of roughly 500 days, so the total mission lasts about 1,000 days.[1] An opposition-class mission uses one low-energy transfer and one high-energy transfer, with a short stay at Mars, typically less than 30 days, so the total mission lasts about 600 days.[1]

The main difference is that conjunction-class missions minimize propellant by accepting a much longer mission and surface stay, while opposition-class missions shorten the stay but require much more propellant because one leg of the trip is high-energy.[1]

Space: Humans to Mars: Fifty Years of Mission Planning, 1950-2000