Saturn V launch vehicle navigation system
Saturn 5 launch vehicle navigation system design, discussing configurations, implementation schemes, system tradeoffs and performance
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Saturn 5 launch vehicle navigation system design, discussing configurations, implementation schemes, system tradeoffs and performance
Linear optimal control and least square filtering theory application to control system design of Saturn 5 launch vehicle
Prediction of forces and heat loads induced by rocket jet plume impingement on Saturn V launch vehicle and launch complex structures
Voyager spacecraft system study - system design and analysis, payload definition, lander design, spacecraft design, sterilization, and shielding
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The Apollo Mission employs more than 210 pyrotechnic devices per mission.These devices are either automatic of commanded from the Apollo spacecraft systems. All devices require high reliability and safety and most are classified as either crew safety critical or mission critical. Pyrotechnic devices have a wide variety of applications including: launch escape tower separation, separation rocket ignition, parachute deployment and release and electrical circuit opening and closing. This viewgraph presentation identifies critical performance, design requirements and safety measures used to ensure quality, reliability and performance of Apollo pyrotechnic/explosive devices. The major components and functions of a typical Apollo pyrotechnic/explosive device are listed and described (initiators, cartridge assemblies, detonators, core charges). The presentation also identifies the major locations and uses for the devices on: the Command and Service Module, Lunar Module and all stages of the launch vehicle.
Saturn I launch vehicle, Saturn IB launch vehicle, and Saturn V launch vehicle components and configuration
Saturn i, saturn ib, and saturn v launch vehicles
Saturn I launch vehicle, Saturn IB launch vehicle, and Saturn V launch vehicle components and configuration
Apollo/Saturn V vehicle launching site, assembly building and lunar flight
Prediction of forces and heat loads of Saturn V vehicle and launch complex environments due to rocket jet plume impingement
Prediction of Saturn V vehicle and launch complex force and heat load environments due to rocket jet impingement - impact pressure and radiation and convective heat transfer
Ability of pilot to stabilize flexibile launch vehicle during first stage - Saturn V launch vehicle
Saturn V launch vehicle malfunction effects model
Mechanical design integration of Saturn S- IVB STAGE of Saturn IB and Saturn V launch vehicle configuration
Functional tests of hydrodynamic system components and flow control valves for Saturn V launch vehicle
Titanium sine wave beam concept for Saturn V launch vehicle
Bending effects on pilot control of simulated flexible Saturn V launch vehicle