Saturn S-4B-507 stage acceptance firing report
Acceptance firing configuration of Saturn S-4B-507 stage
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Protuberance heating test program
Results are presented of the protuberance heating test program. Four general protuberance shapes on a flat plate were tested. Presentation and evaluation of the data both on the protuberance and in the wake regions are made. The test program is an extension of the general protuberance heat transfer test. The additional series of tests was conducted to define the extent of wake heating and to assess the effects of Reynolds number variation on heating both on and around the protuberances. The protuberance models were mounted near the forward end of a six-foot instrumented test plate with stringers that simulated interstage and skirt structure of the Saturn S-4B stage. The tests were performed at Mach numbers of 2.49, 3.51, and 4.44. Reynolds numbers per foot of 3 million and 1.5 million were used for the two lower Mach numbers and 3 million for a Mach number of 4.44. The test Mach numbers simulated the Saturn S-4B flight conditions during the most severe aerodynamic heating period. The test Reynolds numbers were somewhat higher than the flight values, but lower values could not be used because of tunnel and instrumentation limitations. Oil flow runs were made on two representative models at various combinations of Mach number and Reynolds number to help define the extent of wake heating.
Sieker, W. D.↗
Development of the Saturn S-IV and S-IVB LIQUID hydrogen tank internal insulation.
Saturn S-IV and S-IVB liquid hydrogen tank internal insulation, using polyurethane foam reinforced with fiberglass threads
INSULATOR↗
Simulation test report for the S-IVB orbital workshop crew quarters floor and wall grids
Simulated astronaut translational motion across Saturn S-4B stage orbital workshop crew quarters floor and wall grid configurations
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Best estimate method of determining space vehicle ignition and cutoff masses.
Optimal determination of vehicle ignition and cut-off masses, discussing applications to Saturn S-4B Stage flight evaluation
Lenning, J. J.↗
Research achievements review. Volume 3 - Control systems research at MSFC
Servoactuators for Saturn S-4B stage
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A device for measuring the spatial orientation between two separating stages of a space vehicle
Design, development, and testing of device for measuring spatial orientation between separating S-2 and S-4B stages of Saturn 5
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Saturn S-4B-507 narrative end item report
Manufacturing and checkout test data summary for Saturn S-4B flight stage
Reitzell, W. M.↗
Narrative end item report on Saturn S-4B-503 /DAC S/N 1007/
Manufacturing and test data summary for Saturn S-4B flight stage
Morris, J. W.↗
A prime contractor's reliability program for components/parts for the Douglas S-IVB stage project.
Contractor components/parts reliability program for Douglas S-IVB stage project
AIRCRAFT MAINTENANCE↗
Cryogenic quality meter.
Nucleonic cryogenic quality meter design and development and fluid monitoring through hydrogen vent line on Saturn S-IVB stage under orbital conditions
LIQUID HYDROGEN↗
Saturn s-ivb program.
Design requirements of S-IVB stage of Saturn launch vehicle including ground support equipment
ROCKET BOOSTER↗
Chilldown electrical system for s-ivb space vehicle.
Electrical system driving chilldown motor pumps on Saturn S-IVB stage, noting solid state inverter circuitry
SPACECRAFT POWER SUPPLY↗
[Saturn V/S-IVB Stage Low Gravity Fluid Mechanics Problems and Saturn IB Liquid Hydrogen Orbital Experiment to Verify Propellant Ullaging and Orbital Venting System]
Saturn V/S-IVB stage low gravity fluid mechanics problems and Saturn IB liquid hydrogen orbital experiment to verify propellant ullaging and orbital venting system
SATURN IB LAUNCH VEHICLE↗
Saturn s-ivb cryogenic weigh system. iii - environmental control.
Cryogenic tank surface frost control by heated nitrogen for Saturn S-IVB cryogenic weigh system
ICE PREVENTION↗
Use of simulation techniques to remove test- peculiar nonlinear effects from control system response.
Simulation techniques to remove gimbal bearing looseness effect on frequency response and cross axis coupling of Saturn control system S-4B stage
Curtis, H. S.↗
Saturn-S-4B-502 stage flight evaluation report
Postflight data on Saturn S-4B-502 flight
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