Technical development status of the s-ic stage - saturn v launch vehicle.
Technical development status of S-IC stage of Saturn V launch vehicle
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Technical development status of S-IC stage of Saturn V launch vehicle
Saturn V S-IC stage engine guidance, flight control and gimbal servoactuation system for Apollo spacecraft
Feasibility of using liquid fluorine and oxygen /FLOX/ as oxidizer to improve performance of Saturn S-IC stage
Structural analysis, design, and development of titanium alloy skin section for Saturn S-IC STAGE
Electromagnetic compatibility acceptance tests for Saturn S-IC stages
Vibration, shock, and acoustic test requirements and procedures for qualification of Saturn S-IC stage components
Engine and pump inlet duct gimbal joint system in s- ic stage of saturn v launch vehicle
Manufacture of the S-IC stage of the Saturn V space vehicle has resulted in new. concepts and innovations in the field of tooling. The structure size (35-ft diameter), the high reliability and accuracy requirements, and the low density or production quantity lead to a greater degree of simplicity, economy, and versatility in fabrication and assembly tooling. There are three specific concepts which should be applicable in industry, local jigging for welding, rotation of structures in vertical assemblies, and the assembly of two structures. The usual weld jigging serves a two-fold purpose: (a) to support the molten weld puddle and (b) to force and maintain alinement of the parts being welded. The extension of this method to large-diameter tanks is expensive and difficult. An alternate procedure used at MSFC is to perform free-state welding and use local jigging (stra1rclamps) and intermittent tack welding. Cylindrical structures can be accurately rotated for routing or welding on a simplified ring turntable. The tool consists of a ring of the structure diameter resting on rollers. Torque is nearly zero since the ring is rotated by friction rollers with the force being applied at the ring perimeter. Two such turntables are used at MSFC. The horizontal mating of two large components, where controlled motions of small magnitude are necessary, can be easily done by positioning units equipped with air-bearings. Such bearings are usable on concrete of minimum surface preparation and require no special air pressure source. This concept is used in assembly of the two S-IC containers.
Age forming aluminum for center piece head of Saturn S- IC stage
High flow hydraulic filter for engine gimbal system of Saturn S- IC launch vehicle
Summary of study on Saturn IC engine cutoff system model, discrete network simulator model defined, and demonstration of model and computer program simulation of hardware system
Production and fabrication of high pressure helium storage bottles for Saturn S-IC
Hydraulic transformer for pumping oil in Saturn S-Ic vehicle
Titanium alloy skin section for Saturn S-IC FUEL tank
Study of stability of S-IC open loop propellant hydraulic system
Saturn V S-IC electron beam welding system
Environmental controlled areas for fabrication of S-IC space vehicle structures
Modifications on S-IC, S-II, and S-IVB stages of Saturn V launch vehicle