The Space Congress® Proceedings 1968 (5th) The Challenge of the 1970's Apr 1st, 8:00 AM Saturn IB Stage Launch Operations G. Salvador Chrysler Corporation Space Division, Cape Canaveral, Florida R. W. Eddy Chrysler Corporation Space Division, Cape Canaveral, Florida Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Salvador, G. and Eddy, R. W., "Saturn IB Stage Launch Operations" (1968). The Space Congress® Proceedings. 4. https://commons.erau.edu/space-congress-proceedings/proceedings-1968-5th/session-14/4 This Event is brought to you for free and open access by the Conferences at Scholarly Commons. It has been accepted for inclusion in The Space Congress® Proceedings by an authorized administrator of Scholarly Commons. For more information, please contact
[email protected]. SATURN IB STAGE LAUNCH OPERATIONS G. Salvador and R. W. Eddy Chrysler Corporation Space Division Cape Canaveral, Florida Abstract mately 2.5 minutes of operation, it will burn 41,000 gallons of RP-1 fuel and 66,000 gallons of The prelaunch and launch activities are de liquid oxygen, to reach an altitude of approximate scribed as they pertain to the S-IB (booster) ly 42 miles at burnout. H-l engines for later S-IB stage of the 1.6 mi11ion-pound thrust Uprated vehicles will be uprated to 205,000 pounds of Saturn Launch Vehicle. The typical over-all thrust each. schedule for an Uprated Saturn Launch is presented, culminating in the launch, and concluding with The S-IVB stage, with a single 200,000 pound analysis of the data returned.