It amazes me each week when I search for the material for the next post in the rocketry series. The more I look, the more I find of all kinds of interesting facts about the marvelous machine that took the astronauts to the moon. With the technology of today, it should not take long to return to the moon and travel beyond.
This week, we continue our exploration within the Instrument Unit, which is the assembly, perched atop the third stage of the Saturn V. With thousands of gallons of toxic and explosive fuels, and the complexity of the systems that ran the Saturn rocket, it was very important for the safety of the astronauts to have systems in place to monitor and react to any complication that may arise from the spacecraft.
Within the Instrument Unit, there was a section of equipment that was responsible for monitoring the spacecraft systems, the Emergency Detection System (EDS). The primary function of the EDS was to monitor the vehicle during the boost phases of the flight, which was where there was concern for a system malfunction that could cause a failure. The EDS would react in two ways to an alert, it would trigger an automatic abort sequence if a break up was imminent, or if it was a slow failure, it would alert the astronauts by a alarm in the Command Module. Once the decision was made (either manual or automatic) to abort, the process was irrevocable and it went to completion.
The EDS had distribution points and equipment throughout the entire space vehicle. Within the Instrument Unit, the EDS had nine rate gyros located in section 15. These gyros sensed the yaw, pitch, and roll of the vehicle and fed data through the EDS distributor to the flight computer and flight data control signal processor. The EDS distributor monitored data coming in from points throughout the spacecraft and provided alerts to both the astronauts and the ground team.
The EDS distributor also contained the logic analysis systems to process the data necessary for an automatic abort sequence. This system was locked out by a timing circuit that ran for 30 seconds starting at lift off, this would prevent an automatic abort from being initiated that could result in the spacecraft falling back into the launch area. The astronauts did have the ability to initiate an abort sequence manually if there was a two engine cut out during this 30 second window.
Next week, we will look at the radio communications and telemetry instruments. Voice, data, and video feeds kept the ground control stations in constant contact with the astronaut crew. Witnessing the first man to walk on the moon in a live televised event would not be possible without the reliability of the communication systems.