By United States. National Aeronautics and Space Administration. Office of Educational Programs and Services
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Additional info for Launch vehicles
To earth orbit for manned capability for assembly interplanetary ex- ploration. 2. Delivery of passengers lunar missions. 3. Deliver3' e of passengers ing and supplying 4. Direct escape Nova stages will and cargo two stages missions. The height, exclusive of its payload be about 50 feet in diameter. are being and third gen During to the to earth lunar orbit surface for for establish- for orbital vehicle missions will be about and three 300 feet in Fhe first aud seco:ld s,,,ges will Both liquid and solid propellants studied for possible use in the first stage.
Orbit; to Mars or 1965 circumlunar and lunar "Ins dimensions not permit us to show the Advanced relation to the other launch vehicles vanced Saturn, the height also called of the Saturn payload of more powered by five F-l of thrust. powered thrust engine. capable than The C-IB engines second by five J-2 at altitude. With this pounds. lis¢ion is comp:eted, moon to make. rendezvous return journey two-man detached the with the to earth. 5 in the first stage has already of sending the moon. will be Saturn amount engine pounds pounds orbit, engines F-1 with of a single missions.
Direct escape Nova stages will and cargo two stages missions. The height, exclusive of its payload be about 50 feet in diameter. are being and third gen During to the to earth lunar orbit surface for for establish- for orbital vehicle missions will be about and three 300 feet in Fhe first aud seco:ld s,,,ges will Both liquid and solid propellants studied for possible use in the first stage. The second stages will use high-energy liquid-oxygen, liquid-hydro- propellants. powered cargo large space stations.