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...o_Lunar_Module|Lunar Module (LM)]]''' was the lander portion of the Apollo spacecraft built for the US Apollo program to achieve the transit from moon orbit to t [[Category:Spacecraft]] ...

...Module]] into Earth orbit, which made it invaluable for testing the Apollo spacecraft while the larger [[Saturn V]] needed to send them to the moon was still bei [[Category:Spacecraft]] ...

...ere designed to check out procedures and methods to rendevous with another spacecraft, in this case the SIVB. The SPS phase checked out the ability of the SPS to At about T+12min Engine cutoff occurs, the spacecraft is in the almost circular '''Earth Parking Orbit (EPO)'''. ...

...ngine, and is responsible both for the final part of the launch to put the spacecraft in orbit, and for the [[TLI]] burn to boost them on a trajectory that will [[Category:Spacecraft]] ...

...nd_Module_.28CM.29|Command Module (CM)]] is the nerve center of the Apollo spacecraft, as it functions as primary control and navigation platform during the miss ...ut are really doing what the original switches did. So you can operate the spacecraft as the real astronauts did, at least the more important subsystems. Additio ...

..."Apollo 11 - Assembly"''' scenario in the "Project Apollo - NASSP\Apollo - Historical Missions\Apollo 11" folder. The Mobile Launcher (ML) and Launch Umbilical T [[Image:Apollo_spacecraft_stacking.jpg|thumb|right|Stacking of the Apollo spacecraft in the VAB.]] ...

At about T+12min Engine cutoff occurs, the spacecraft is in the almost circular '''Earth Parking Orbit (EPO)'''. You can control The scenarios for an Apollo 11 Standard mode mission are in the '''Apollo - Historical Missions\Apollo 11''' folder. The following table shows the currently avail ...

...115V AC power, and a 10Hz signal from the central timing equipment in the spacecraft. It can operate by using an internal tuning fork as a reference if the timi ...count down to liftoff, and as far as we can determine this is the correct historical behaviour. ...

...ndicator (FDAI)''' is used to display various attitude informations of the spacecraft, similar to a artificial horizon of an aircraft. The FDAIs provide displays ...read "pitch 0°", "bank 0°" and "ball centered") is not necessary when the spacecraft is nose on the horizon, "wings" at level and pointing toward the heading. ...

...ors, as well as read up any PAD that is pertinent to upcoming maneuvers at historical points in the mission’s Flight Plan. The MCC is currently functional for ...ations have Acquision of Signal (AOS) or Loss of Signal (LOS) based on the spacecraft’s ground track and whether or not it is on the far side of the moon. Curr ...

* All types of IMU transformation matrizes (REFSMMAT) used for the Apollo spacecraft. ...FSMMATs can be calculated by the AGC itself, but most were uplinked to the spacecraft from the ground. The REFSMMATs that can be calculated with this MFD are: ...

...itions to the spacecraft simulated in '''Project Apollo''' after the basic historical [[Command/Service Module]] and [[Lunar Module]] are complete. ==Spacecraft== ...