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- ...therwise: P64 -> P67!); Final steering (P67 w. N66); End of steeering (P67 w. N67) ...9 KB (1,628 words) - 20:11, 5 June 2011
- '''[[w:Apollo_7|Apollo 7]]''' was the first manned mission in the Apollo program w ...4 KB (685 words) - 16:27, 30 January 2017
- ...controlled with [[w:Nitrogen|nitrogen]]. The engine is gimbaled to allow [[w:Thrust vectoring|Thrust Vector Control (TVC)]] during a burn. ...PS GIMBAL meter can be used to trim the CSM to compensate changes of the [[w:Center_of_mass|center of mass]], however this is not necessary in Project A ...22 KB (3,818 words) - 11:01, 29 July 2008
- ...W of heating each. Additionally the suit is heated by the crew at about 10 W per crew member. ...der to heat or cool the coolant loops manually. You can add or remove 3000 W of heating to or from each loop. With the following procedure you can disco ...9 KB (1,529 words) - 23:56, 19 December 2006
- ...e AGC (the CSM [[AGC]] controls the burn) or the Project Apollo MFD (the [[w:Saturn_V_Instrument_Unit|S-IVB IU]] controls the burn). ...6 KB (1,008 words) - 17:09, 27 September 2007
- ...f the Integrated Manned Program was the Reusable Nuclear Shuttle(RNS), a [[w:NERVA|NERVA]] based propulsion stage that could be used either to shuttle c * J.P. Downs, W.B Thompson, ''[http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/1979007 ...11 KB (1,553 words) - 00:14, 26 July 2011
- ...h resets the master alarm. This switch-light is not illuminated when the C/W system is in boost mode to avoid confusion with the ABORT button. </td> ...ch-light on the main panel will not illuminate. When switched to ACK the C/W status lights will illuminate only when a master alarm switch-light is pres ...44 KB (7,630 words) - 16:30, 13 October 2006
- * LOI-1 (w/ MCC): A special mode for the LOI-1 calculation, necessary for LOI-2 REFSMM * LOI-1 (w/o MCC): The normal case for the Lunar Insertion Maneuver 1. The goal for L ...21 KB (3,364 words) - 13:29, 17 February 2017
- ...nce to the X-Matrix when using a alternate line of sight for marking. (See W-Matrix) ...: Defines Rendezvous positional variance using optical sighting marks (See W-Matrix) ...15 KB (2,236 words) - 15:42, 7 July 2011
- ...carry freight and six astronauts into orbit in support of Earth orbital [[w:Apollo Applications Program | Apollo Applications Program]] missions. ...on a Titan/Agena booster which could be used to rescue the crew from an [[w:Apollo Applications Program | Apollo Applications Program]]-based space sta ...89 KB (13,330 words) - 11:56, 19 March 2013