User:Rjg77vett/Sandbox

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Article II

It is important for those interested in the lift capabilities of rockets like the Saturn and Nova series to see a side-by-side comparison of these rockets alongside the vehicle that the USA has been using for the past two decades, the Space Shuttle System. This will clearly reveal how poor the planning has been, not only for earth orbit capability, but for moon/planetary exploration.

More information Parameter, Atlas ...
Parameter Atlas Titan II Saturn I Saturn V Nova Space Shuttle Energia (Russia)
Date of Last Launch 1963 1965 1966 1974 N/A In Progress 1998
Stages 2 2 3 5 5 3 5
Stage I Engines 3 3 5 F-1 (5) F-1 (8) x-z (2) row 2, cell 8
Thrust at Launch (lbs.) 300,000 425,000 1.5 Million 7.5 Million 12 Million 1.5 Million 12 Million
Earth Orbit Payload (100 mi) Tons Tons Tons Tons Tons Tons Tons
Earth Orbit Payload (300 mi) Tons Tons Tons Tons Tons Tons Tons
Luner Trajectory (25 km/h) Tons Tons Tons Tons Tons Tons Tons
Close

One ton=2,000 lbs.
one pound = 0.4536 kilograms (approx.)
Rjg77vett (talk) 22:28, 13 January 2009 (UTC) End of Article II


Article I

Carlton Godfrey

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