Labels:text | black and white | screenshot | diagram OCR: MISSION PERFORMANCE SUMMARY - MARS MISSIONS 3.07 #Electric Propulsion Assumptions : low-thrust trajecto- + 2007 Opportunity Chemical ry trip times not + "500 Day " Class Missions 2.51 equivalent to impul- with Venus Swing-by. sive thrust trip times #Minimum Energy Missions * Trip Time/Payload Constant 2.0+ Chemical/ Aerobrake "500 Day" with Venus Swingby Minimum Energy 1,5 Nuclear Nuclear / Thermal +Nuclear Solar 1.01 .Thermal Nuclear Electric # Thermal (Gas Core) 0.5 0.0' 475 475 850 1200 2500 Isp (seconds) 6000
