Use of AGS[edit]
There are few actual descriptions of the use of the AGS, as a landing abort was never needed during the Apollo missions. There were, however, four cases in which the AGS was used.
Its first use was for testing of the Lunar Module descent stage in Earth orbital flight during the
Apollo 9 mission
[6]. It was used again in the
Apollo 10 mission, following separation of the Lunar Module descent stage prior to the APS burn. An incorrect switch setting
[7] leaving AGS in
Auto rather than
Attitude Hold mode led to a prompt and pronounced deviation in attitude moments before staging
[8]. The situation was quickly brought under control.
The next use of the AGS was during the lunar ascent phase of the
Apollo 11 mission, when the LM crew performed a sequence of rendezvous maneuvers that resulted in
gimbal lock; the AGS was subsequently used to acquire attitude control.
[2]
The AGS played an important role in the safe return of
Apollo 13 after an oxygen tank explosion left the Service Module crippled and forced the astronauts to use the Lunar Module as a "lifeboat." Supplies of electrical power and water on the LM were limited and the Primary Guidance and Navigation System used too much water for cooling. As a result, after a major LM descent engine burn 2 hours past its closest approach to the Moon to shorten the trip home, the AGS was used for most of the return, including two mid-course corrections.