Figure 8.20 Nuclear Electric LTV The specific impulse (Isp) of electric propulsion systems are given in Table 8.10. _____ Table 8.10 Propulsion System Performance for Future Applications Figure 8.21 shows the initial LEO mass for different propulsion technologies. The mission profile used for this study assumes that a payload of 35000 kg is delivered from LEO to LLO and no payload is returned. This Figure also gives the trip time for that mission. Figure 8.21 Propulsion Technology Comparison and Trip Time Round Trip (LEO-LLO) - Payload Mass : 35 Tones
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