lunar module optical rendezvous system
1Lunar Module — Module lunaire Apollo Pour les articles homonymes, voir LEM et LM. Module lunaire du programme Apollo …
2Module Lunaire — Apollo Pour les articles homonymes, voir LEM et LM. Module lunaire du programme Apollo …
3Module lunaire — Apollo Pour les articles homonymes, voir LEM et LM. Module lunaire du programme Apollo …
4Module lunaire Apollo — Pour les articles homonymes, voir LEM et LM. Module lunaire du programme Apollo Dimensions …
5Abort Guidance System — (AGS) was a backup computer system in Apollo Lunar Module. It was completely different computer system than Apollo Guidance Computer (AGC) because it was designed by TRW independently from the AGC development. This computer system was intended to …
6Primary Guidance, Navigation and Control System — Das Primary Guidance, Navigation and Control System (PGNCS (ausgesprochen: pings)) war das unabhängige inertiale Navigationssystem der Apollo Raumfahrzeuge. Es ermöglichte den Apollo Raumfahrzeugen die Durchführung ihrer Operationen bei… …
7Alunisseur — Module lunaire Apollo Pour les articles homonymes, voir LEM et LM. Module lunaire du programme Apollo …
8Apollo PGNCS — The Apollo Primary Guidance, Navigation and Control System (PGNCS) (pronounced pings) was a self contained inertial guidance system that allowed Apollo spacecraft to carry out their missions when communications with Earth were interrupted, either …
9Apollo spacecraft — The Apollo spacecraft was designed as part of the Apollo Program, by the United States in the early 1960s to land men on the moon before 1970 and return them safely to earth. This goal was set forth by President Kennedy after the first flight of… …
10Apollo 15, Return to Earth — After the Apollo 15 Lunar Module Falcon lifted from the lunar surface it rendezvoused and docked with the Command/Service Module Endeavour . After transferring across the lunar samples and other equipment, Falcon was jettisoned. It would fire its …
