The ST-124-M3 inertial platform was a device for measuring acceleration and attitude of the Saturn V launch vehicle. It was carried by the Saturn V Instrument Unit, a 3-foot-high (0.91 m), …

The Saturn V instrument unit is a ring-shaped structure fitted to the top of the Saturn V rocket's third stage and the Saturn IB's second stage (also an S-IVB). It was immediately below the …

A review of the navigation, guidance, and control system of the Saturn launch vehicle includes the system analysis and design, signal flow diagrams, redundancy, and self-checking features …

This is an unflown example of a Stablized Platform, which was used to guide and control the Saturn V rocket. It contained within it a set of gyroscopes and accelerometers, which …

the Saturn V dynamic test are plotted in figure 6 as a function of bend- ing moment. The local deflection is taken as the difference between the gyro readings at the top half of the EDS cold …

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 …

The document describes the ST-124M inertial stabilized platform system and its application to the Saturn V launch vehicle. It provides a system concept description of the platform, its …

The ST-124-M3 inertial platform was a device for measuring acceleration and attitude of the Saturn V launch vehicle. It was carried by the Saturn V Instrument Unit, a …

1970年3月1日 · The navigation and control information is obtained inertinlly by a gyro-servo-stabilized, three-gimbal platform system with three mutually orthogonal pendulous-integrating …

2023年2月25日 · The entire Saturn V rocket was controlled by the instrument unit, located at the top of the 3rd stage. It contained the inertial guidance platform, an advanced mechanical …