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Apollo 5 Mission Lunar Module Test pt1-2 1968 NASA color 7min

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Published on Sep 21, 2011

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NEW VERSION: http://www.youtube.com/watch?v=Po178H...
has improved sound, all in 1 part.

Apollo 5 (SA-204, Saturn-Apollo 204) was an unmanned test of the Lunar Module for Project Apollo. A Saturn I-B launch vehicle was used to launch the LM into Earth orbit.

This is an Improved version of a previous upload with letterboxing (black borders) removed and aspect ratio corrected. NASA film JSC-461

Launch date January 22, 1968 22:48:09 UTC
Mission duration 11 h 10 m

part 2: http://www.youtube.com/watch?v=AQ-id3...

NASA Apollo 5 Mission Report:
http://ntrs.nasa.gov/archive/nasa/cas...

hi-res photo: APOLLO 5 SATURN [SA-204] FIRST STAGE IS HOISTED AT LAUNCH COMPLEX 37B FOR MATING TO SECOND STAGE
http://images.ksc.nasa.gov/photos/196...

Wikipedia
Apollo 5 was the first unmanned flight of the Apollo Lunar Module, which would later carry astronauts to the lunar surface. It lifted off on January 22, 1968 with a Saturn IB rocket.

The Apollo 5 mission tested the Lunar Module in a space environment, in particular its descent and ascent engine systems, and its ability to separate the ascent and descent stages. The descent engine would become the first throttleable rocket engine fired in space.

The mission also performed a "fire in the hole" test (as depicted in the mission's insignia) in which the ascent stage engine would be fired while still attached to the descent stage. This was intended to simulate a landing abort during descent to the lunar surface.

As with Apollo 4, this flight experienced long delays. The primary cause of this was the Lunar Module, which was well behind schedule. Some of the delay could be attributed to lack of experience in building a manned spacecraft to land on the Moon.

The first unmanned launch was originally planned in April 1967, requiring delivery at the Cape around September 1966. But delays kept occurring. Although the Lunar Module was fully designed, there was trouble fabricating the custom made parts. The engines were also having problems. The descent engine was not burning smoothly, and the ascent engine was having fabrication and welding difficulties.

In the end these problems were overcome, but it took several months and it was not until June 23, 1967 that the Lunar Module arrived at the Cape on board Aero Spacelines' Super Guppy. After four months of tests and repair the Lunar Module was mated to the launch vehicle on November 19...

The launch vehicle for Apollo 5 was the Saturn IB, a smaller rocket than the Saturn V but capable of launching an Apollo spacecraft into Earth orbit. The Saturn IB SA-204 used on Apollo 5 was the one originally intended for Apollo 1.[1] It had been undamaged in the fire at Launch Complex 34 and was reassembled at Launch Complex 37B for the Apollo 5 launch.

The windows of LM-1 were replaced before the flight with solid aluminum plates. To hasten delivery, it was decided to do without the Lunar Module's legs. Without a crew or CSM, there was no need for a launch escape system. As a consequence the assembled rocket was 55 meters (180 ft) tall, compared to the usual CSM stack height of 68 meters (223 ft).

On January 22, 1968, Apollo 5 lifted off just before sunset. The Saturn IB worked perfectly, inserting the second stage and LM into a 163 x 222 km orbit. The nose cone was jettisoned and after a coast of 43 minutes 52 seconds, the LM separated from its adapter, with a 167 x 222 km orbit. After two orbits, the first planned 39 second descent engine burn was started, but aborted by the onboard guidance computer after only 4 seconds. Shortly before launch there was a suspected fuel leak and a decision was made to delay arming the engine until the time of ignition. [2] This change had increased the time required for the propellant tanks to pressurize and thrust to build to the required level.

The ground controllers moved to an alternate plan to fire the descent engine manually two more times. They then performed the "fire in the hole" test and another ascent engine burn.

After 11 hours and 10 minutes the test was over, and control of the two stages was terminated. The stages were left in a low enough orbit that atmospheric drag would soon cause their orbits to decay and re-enter the atmosphere. The ascent stage (1968-007A) re-entered on January 24 and burned up; the descent stage (1968-007B) re-entered on February 12, falling into the Pacific several hundred kilometers[specify] southwest of Guam.[citation needed]

Despite the descent engine programming error, NASA deemed the mission a success in demonstrating the LM systems, and a second unmanned flight test using LM-2 was canceled. LM-3 was cleared for the first manned flight, which occurred on Apollo 9.
http://en.wikipedia.org/wiki/Apollo_5

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