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"Some computer applications in Saturn stage checkout."
This paper discusses a number of interesting applications of digital computers in the checkout of individual Saturn stages and in the prelaunch checkout of the complete Saturn vehicle. It discusses the concepts of automation in Saturn checkout, the unique two-computer mode of operation at the launch site and the operations of the high speed data link connecting the two computers. Also discussed are the functions of the computer while propellants are loaded automatically on one of the stages; the functions of the display computer in the newest and largest Saturn display system, and operations and utilization of the Digital Events Evaluator, the main recording device utilized during stage checkout. -
"Spacecraft television ground data handling system."
A design report which displays and explains how the Spacecraft Television Ground Handling System functions, is designed and what it might be used for in the future. -
"Stability analysis of Apollo - Saturn V propulsion and Structure feedback loop."
The propulsion and the structure of a space vehicle form a feedback loop through inertial coupling referred to as the pogo phenomenon and experienced with the Thor , Titan, and Apollo-Saturn V space vehicles. -
"Saturn V S-IC stage engine gimbal actuation system."
The actuation system for the Saturn V S-IC stage is described and compared to the Saturn I system. The use of mechanical feedback actuators that result in a significant increase in system reliability and the damping of load resonance is discussed. The unprecedented component sizes and system requirements are cited. -
"Saturn V vehicle electronics."
This presentation is a review of the electrical and electronics systems of the Saturn V launch vehicle. Since airborne and ground electronics cannot be separated as a system, this presentation will touch upon both the airborne and ground checkout equipment. Certain airborne electronic items are singled out in order to elaborate upon the application of computers for checkout and launch. This review covered in a broad sense such airborne electronics as the control computer, the measuring telemetry and RF systems, the switch selector, the digital command receiver and the remote automatic calibration system. The ground support equipment electronics covered include such equipment as the data link, computer system and display systems. The importance of software in the Saturn V program is stressed by the application of a standard program language through the use of acceptance test or launch language (ATOLL). -
"Saturn V S-IC stage engine gimbal actuation system."
The actuation system for the Saturn V S-IC stage is described and compared to the Saturn I system. The use of mechanical feedback actuators that result in a significant increase in system reliability and the damping of load resonance is discussed. The unprecedented component sizes and system requirements are cited. -
"Saturn V vehicle electronics."
This presentation is a review of the electrical and electronics systems of the Saturn V launch vehicle. Since airborne and ground electronics cannot be separated as a system, this presentation will touch upon both the airborne and ground checkout equipment. Certain airborne electronic items are singled out in order to elaborate upon the application of computers for checkout and launch. This review covered in a broad sense such airborne electronics as the control computer, the measuring telemetry and RF systems, the switch selector, the digital command receiver and the remote automatic calibration system. The ground support equipment electronics covered include such equipment as the data link, computer system and display systems. The importance of software in the Saturn V program is stressed by the application of a standard program language through the use of acceptance test or launch language (ATOLL). -
"Saturn V : non-stage procured launch vehicle ground support equipment."
The functions, authority, management relationships, and responsibilities of the Launch Vehicle Ground Support Equipment Project Office are described. Functions and examples of non-stage procured Launch Vehicle Ground Support Equipment (LVGSE) are described and illustrated.