Apollo status report - Saturn V launch vehicle.
Saturn 5 launch vehicle design, role in exploration and anomalous structural vibration and oscillation
James, L. B.↗
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Analog sensitivity design of Saturn V launch vehicle
Saturn 5 launch vehicle control system optimal desensitization with feedback, using analog computer for sensitivity design
Rillings, J. H.↗
The saturn v launch vehicle.
Design approach, testing and checkout program of Saturn V launch vehicle
LAUNCH VEHICLE↗
Saturn V Launch Vehicle Digital Computer and Data Adapter
Saturn V launch vehicle digital computer and data adapter for checkout and guidance functions
DATA CONVERTER↗
The s-ii stage of saturn v launch vehicle.
S-II stage of Saturn V launch vehicle, its mission, stage systems, structural components and fabrication techniques
APOLLO PROJECT↗
The aeroelastic characteristics of the Saturn-IB and Saturn-V launch vehicles
Effects of flow separation on aeroelastic characteristics of Saturn IB and Saturn V launch vehicles with Apollo payload
FLOW SEPARATION↗
Technical development status of the s-ic stage - saturn v launch vehicle.
Technical development status of S-IC stage of Saturn V launch vehicle
SATURN V LAUNCH VEHICLE↗
Modified launch vehicle /mlv/ saturn v improvement study composite summary report
Modifications on S-IC, S-II, and S-IVB stages of Saturn V launch vehicle
SATURN S-I STAGE↗
Saturn V launch vehicle systems analysis application.
Systems analysis applied to identification of Saturn V launch vehicle support system requirements and establishment of baseline logic for vehicle prelaunch processing simulation and systems optimization
SYSTEMS ANALYSIS↗
Application of the Saturn V launch vehicle to unmanned scientific exploration of the planet Jupiter.
Saturn V launch vehicle and Apollo spacecraft hardware systems applied to unmanned exploration of Jupiter
APOLLO SPACECRAFT↗
Advanced control systems for the Saturn V launch vehicle.
Adaptive control systems for stabilizing structural bending modes of Saturn V launch vehicle
VIBRATION MODE↗
Voyager spacecraft system study /phase II SATURN V launch vehicle/, volume IIb Final report
Voyager spacecraft system design and analysis - Saturn V launch vehicle
SPACECRAFT DESIGN↗
Voyager spacecraft system study. Phase II - Saturn V launch vehicle. Volume I - Summary Final report
Voyager spacecraft system using Saturn V launch vehicle - summary of parametric studies for unmanned exploration of Mars by landing module
UNMANNED SPACECRAFT↗
Piloted guidance and control of the Saturn V launch vehicle.
Man-machine system in control and guidance of Saturn V launch vehicle, emphasizing participation during atmospheric phase of flight profile
ROCKET INSTRUMENTATION↗
Electrical support equipment for the saturn v launch vehicle system.
Electrical support equipment and digital computer descriptions and functions in Saturn V launch vehicle checkout
DIGITAL COMPUTER↗
Saturn V launch vehicle report.
Ground testing, development of engines, stages and ground support equipment of Saturn V launch vehicle
GROUND SUPPORT EQUIPMENT↗
A design study of a helium recovery system for mila. volume iii- helium usage and recovery equipment supporting data
Design study for helium usage and recovery equipment in Saturn V launch vehicle
SATURN V LAUNCH VEHICLE↗
The Enduring Legacy of Saturn V Launch Vehicle Flight Dynamics and Control Design Principles and Practices
It has been over 50 years since the first launch of the Saturn V launch vehicle, Apollo 4, on November 9th,1967. Developed at NASA’s Marshall Space Flight Center (MSFC) in Huntsville, Alabama, the Saturn V was a massive multistage liquid-fuel expendable rocket used by NASA’s Apollo and Skylab programs. It safely flew 24 American astronauts to the Moon, blazing the trail for all American heavy-lift launch vehicles to follow. The Saturn V remains the only launch vehicle to carry humans beyond low Earth orbit. Nearly fifty years after the final May 1973 flight of the Saturn V, an enduring technical legacy of launch vehicle technologies still supports the United States space launch capabilities, particularly with respect to flight dynamics and control. The structured refinement of GN&C technologies during the Saturn program, leveraging the incremental advancements of the Jupiter, Redstone, and Saturn I/IB, systematically reduced risk and resulted in the most advanced and reliable launch vehicle flight control systems to have been developed before the advent of the Space Shuttle.
Jeb S Orr↗