First, Table I showing the orbital parameters for a Venus flyby launch, first into 100 nautical mile parking orbit, then doing a second burn of the S-IVB into a 48 hour 70,000 mile high elliptical orbit as phase 1 of the Trans-Venus Injection maneuver...
Second, Table II, the weight summary of the launch vehicle and spacecraft...
Third, Table III, performance of the Saturn V into a 70,000 nautical mile elliptical orbit...
Fourth, Table IV, Trans-Venus Injection dates for a Venus flyby mission...
Fifth, Mars preliminary flyby payload, used in lieu of a Venus payload since no payload planning for a Venus flyby had been done to this point...
Sixth, the Venus flyby vehicle in Trans-Venus Injection configuration for the trip to Venus...
More to come! OL J R
