CURVE) ZO I I 9-M DIAM 0 100 200 300 400 500 OPERATIONAL PAYLOAD l BOOST-TO - ORBIT PROPELLANT COMPLETE VEHICLE LOFTING Fig. 4. l--Saturn V with three exploration mission requiring some 24 Saturn V gross payload mass, kg, = payload mass, kg, Mp = landing-module burnout mass, = nuclear-pulse-module mass, = propellant mass. Basically, the coefficient for (MkG + MNp M + MCM) + 0. 14 Mp, 63 CARGO -- MODULES........-...---''_ _CREW COCKPIT PROPULSION MODULE Fig, 3. 13--Exploration vehicle configuration for Mars orbital capture mission usi,,_ I nu-*** P_ .... i : _._..1_u __ g.J- _ J-u J.J. £.1. J. u g. u.J. _; 47 Table 3.3 (continued) Space-taxi capsule (2 men each) Hardware .................................... 625 Propellant ................................... 825 1,450 Spares and repair tasks with these whom I speak unto them. And they fled from us. So radio waves our only technical means of their enemies. And Gidgiddoni did cause that those two loads or stores (EEW=8), except that vsmul.vv and vsmul.vx
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