The Apollo Guidance & Navigation system was the state of the art in its day, it was, and still is a marvellous construction that performed with peerless reliability. As its name implies, and describing it in the crudest terms, it was a system to control where and when a rocket or spacecraft would be at any one given time, you told it where and when you wanted to be and it would take you there. When describing the Apollo guidance computer there is what appears to be an irresistible urge in the most for people to make the overused parallel that a modern smartphone has more memory/processing power than the computer that flew man to the moon. Whilst this may be true it should not be forgotten that this system was made for a singular purpose, and it carried it out admirably. The system was designed & built by the Massachusetts Institute of Technology a private research University, and was a departure from NASA’s usual method of awarding manufacturing contracts to industrial companies.
Before any space agency will allow a human to ride in a rocket a rigorous set of tests and trials are carried out to man-rate the equipment. It should always be remembered that when president Kennedy challenged the American nation with the goal of sending men to the Moon, he included the words “and returning them safely”. Apollo was no exception to the rule and an enormous amount of time and money was expended working on the safety and reliability of the hardware.
To achieve this there were a series of unmanned test flights in the Apollo program, one of which was AS-202. It was aboard this spacecraft that the first fully functioning Apollo Guidance & Navigation system was flown. Also installed and flown for the first time were the fuel cells which supplied the electrical power supplies to the spacecraft.
In keeping with NASA procedures after a test flight most of the recovered hardware would be returned to the manufacturer for evaluation. NASA documents indicate that flown hardware components were to be marked in a particular manner to identify them. After this evaluation large amounts of this used hardware were consigned to be sold off as scrap.
This is where Jimmie Wayne Loocke steps into the story, he was fortunate enough to have bought a large job-lot of ex-NASA hardware from a scrap merchant in the mid 70’s, who in turn had won the items in a GSA auction at NASA JSC
Amongst this treasure was an Apollo Block 2 Guidance & Navigation computer, which Jimmie and a team of experts that he assembled, have restored to be fully functioning. During the restoration it was determined that the AGC was used in LTA-8 during the first man rating of the LEM.
Jimmie has a great website that follows the restoration, and is well worth a visit
Click on the link to the right to take you to Jimmies site
Alternatively you can access the site directly from the embedded page below
Amongst other items were a nearly complete set of electronic modules from the guidance system of AS-202. These have been identified as such by the markings they bear and the serial numbers on the disposal paperwork match NASA documentation.
The module I have took electrical signals from the computer, amplified them and sent them to control the gyroscope. This gyroscope was part of the Inertial Movement Unit which sensed where the vehicle was in space relative to a known point. The module bears the triangular NASA quality control stamp, and more importantly is marked in yellow lettering Flight 202.
Front face of the module.
For a sense of perspective it is 100mm (4") long by 50mm (2") wide by 65mm (1.3") tall and weighs 50 grams (2oz)
The bottom face, showing the pin connectors
The back face, showing the threaded holes where the fixing screws held the module into the PSA tray
The module is shown here still installed in PSA tray Number 1
A page from a system manual, this page shows the contents of tray Number 1. Here it can be seen that the part number of 1007540 is shown, the manual is a slightly different version and that is reflected in the fact that the module is revision -011 and the manual shows revision -021.
A description of the modules function is given as- Demodulates and amplifies inner gimbal error signals and supplies correction signals to inner gimbal torque motor
Here is a schematic showing the 10 trays that made up the complete Power Servo Assembly, the module can be seen listed in tray 1
This illustration shows the physical location of the PSA trays
Post flight photos of the Command Module interior, the first is marked showing the PSA tray location. The electronics have been stripped out and sent back to the manufacturers for evaluation
The following images show the module being removed from PSA tray Number 1
Jimmie and his colleagues have carried out searches and pieced together information that confirms that the modules are the actual ones that were flown on the mission.
This clip was from a document and shows that the PSA tray flown on flight AS-202 was Serial No1
After the flight the Command Module was stripped, and the items were returned to the respective manufacturers for evaluation. After this was carried out the items were then returned to NASA. Below is the front page of Document No 10717 showing that A/C Electronics were returning Apollo equipment to NASA.
This is the second page of Document No 10717, Line item No 15 shows PSA tray No1, which was serial No1. This confirms that the module has come from the flown tray. These items were stored away by NASA and around about the cecessation of the Apollo program in the mid seventies NASA disposed of the items by selling them to scrap merchants
A further proof is contained in this document relating to the marking of components. It specifies that flight items are to be marked with the flight number in yellow text. This is clearly seen on the module
Drawings of the Module
Flight AS-202
The flight launched at 12.15 p.m. EST on the 25th August 1966. The flight lasted 1hr 33 minutes, it was a complete success.
The Launch vehicle & spacecraft comprised of the following
Saturn 1b first Stage
S-IVB second Stage
Innstrument Unit (IU)
Spaceccraft LM Adapter (SLA)
Block I Command & Service Module
Launch Escape System (Including a Blast Protective cover-BPC)
There were a long list of mission objectives, the most noteworthy being the first time that an Apollo spacecraft drew its electrical power from fuel cells. The SPS engine that would eventually propel the CSM and LM to the moon and back was successfully restarted multiple times. The Apollo Guidance and navigation system had its first workout. The flight went a long way in qualifying various systems for manrating