This was the first flight of the Saturn V, the largest launch vehicle ever constructed. It was also the first launch from Launch Complex 39 specifically built for the Saturn V. As well as being the first launch of the S-IC first stage and S-II second stage, it would also be the first time that the S-IVB third stage had been restarted in Earth orbit and the first time that the Apollo spacecraft had reentered the Earth's atmosphere at speeds approaching those of a lunar return trajectory. Because of all these firsts there were 4,098 measuring instruments on board the rocket and spacecraft.
This would be the first test of the all-up doctrine. It had been decided in 1963 that instead of testing each component of the rocket separately like had been done by Wernher von Braun in Germany during World War II, the rocket would be tested all at once. This cut down the total number of tests, as needed to accomplish President Kennedy's stated goal of a manned lunar landing by 1970, but it meant that everything had to work properly the first time. Apollo program managers had misgivings about all-up testing but agreed to it with some reluctance since individual component tests would inevitably push the landing mission past the 1970 goal.
There were two main payloads on board. CSM-017 was a production model of the spacecraft that would take the astronauts to the moon. It was a Block I spacecraft meant for testing the systems, and not the Block II spacecraft that would be actually manned. However it did feature some Block II items such as an improved heatshield and a new hatch. The other payload was LTA-10R which was a model of the Lunar Module carried as ballast but with the same mass distribution as the real craft.
The Command and Service Module (CSM) arrived at the Cape on Christmas Eve 1966, followed by the second stage on 12 January 1967. Only two weeks later the fatal fire in the Apollo 1 spacecraft occurred pushing all the schedules back. An inspection of wiring in the CSM found 1,407 problems.
The stacking of the S-II took place on 23 February. This was a precision process; supposedly the crane operators could conceivably "lower the crane hook on top of an egg without breaking the shell". The piece had to be unstacked after hairline cracks were found in another S-II. The CSM was finally ready as well and on 20 June it was mated to the rocket and the whole launch vehicle rolled out of the VAB on 26 August - six months after the originally scheduled launch date.
After a testing regime that lasted two months the rocket was finally ready for launch. The propellant started being loaded on 6 November. In total there were 89 trailer-truck loads of LOX (liquid oxygen), 28 trailer loads of LH2 (liquid hydrogen), and 27 rail cars of RP-1 (refined kerosene).
The five F-1 engines sent a huge amount of noise across Kennedy Space Center. To protect from a possible explosion, the launch pads at LC-39 were nearly four miles from the Vehicle Assembly Building. However, the noise was much stronger than expected and buffeted the VAB, firing room and press buildings. Ceiling tiles fell around Walter Cronkite in the CBS news booth. NASA later built a sound suppression system that pumps thousands of gallons of water onto the flame trench under the pad. A similar system is still used today with Space Shuttle launches.
The perfect launch placed the S-IVB and CSM into a 185 kilometer orbit. After two orbits, the S-IVB reignited for the first time, putting the spacecraft into an elliptical orbit with an apogee of more than 17,000 kilometers. The CSM separated from the S-IVB and fired its Service Propulsion System (SPS) engine to send it out to 18,000 kilometers. Passing apogee, the Service Propulsion System fired again to increase re-entry speed to 40,000 km/h, simulating a return from the moon.
The CM landed 16 km from the target landing site. Its descent was visible from the deck of the USS Bennington, the prime recovery vessel.
A compilation of original NASA footage shows the jettisoning of the first stage (S-IC) and the interstage, filmed from the bottom of the second stage (S-II), both from Apollo 4. This is followed by footage of the separation of an S-IVB second stage from the S-II second stage of Apollo 6. The glow seen on the jettisoned stages is due to the hot, invisible hydrogen-oxygen flames of the J-2 engines used by the S-II and S-IVB. The footage also shows the more conspicuous plumes of the solid ullage motors as they pull the stages apart before the main engines are fired.
The cameras ran at 15 times normal speed to show the events in slow motion. The camera capsules were jettisoned soon after the first stage separation and though at about 200,000 feet in altitude, were well below orbital velocity. They then reentered the atmosphere and parachuted to the ocean where they floated waiting for recovery. Both S-II cameras from Apollo 4 were recovered so that there is footage from both sides of the vehicle.
WIPO ASSIGNS PATENT TO SOLYSTIC FOR "DEVICE FOR UNSTACKING FLAT OBJECTS THAT DETECTS THE PATH OF UNSTACKED OBJECTS" (FRENCH INVENTORS)
Jan 23, 2011; GENEVA, Jan. 23 -- Publication No. WO/2011/007077 was published on Jan. 20. Title of the invention: "DEVICE FOR UNSTACKING FLAT...