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  • #REDIRECT [[w:S-IC]] ...
    20 bytes (3 words) - 13:27, 14 December 2006
  • ...flight of the Saturn V launch vehicle. It was also the first flight of the S-IC and SII stages of the rocket. ...
    689 bytes (97 words) - 23:47, 25 October 2006
  • ...pollo Saturn V launch vehicle. An interstage would be fitted on top of the S-IC stage to support the S-IVB stage, so it could be considered either a souped ...
    865 bytes (138 words) - 13:10, 26 October 2007
  • The '''[[w:Saturn_V|Saturn V]]''' (pronounced 'Saturn Five,' popularly known as the Mo The rocket consists of three stages. The [[S-IC]] has five [[F-1]] engines, burning liquid oxygen and kerosene, the [[S-II] ...
    3 KB (557 words) - 13:12, 1 November 2007
  • #REDIRECT [[w:S-IB]] ...
    20 bytes (3 words) - 15:46, 14 December 2006
  • #REDIRECT [[w:S-II]] ...
    20 bytes (3 words) - 14:57, 12 October 2007
  • #REDIRECT [[w:S-IVB]] ...
    21 bytes (3 words) - 15:07, 12 October 2007
  • Project Apollo simulates the Block II '''[[w:Apollo_Command/Service_Module|Command/Service Module (CSM)]]''', providing ...tform during the missions. It houses the highly-advanced (for the 1960s) [[w:Apollo_Guidance_Computer|Apollo Guidance Computer]], as well as all the sys ...
    5 KB (787 words) - 21:36, 14 January 2017
  • The '''[[w:Crawler-transporter|Crawler Transporter (CT)]]''' is the most important ves * At T-30s the S-IC Intertank Arm is retracted. ...
    5 KB (842 words) - 20:16, 12 May 2007
  • The '''[[w:Saturn_1b|Saturn IB]]''' was used to launch the Apollo 7 mission, ASTP miss ...
    1 KB (207 words) - 18:26, 10 October 2007
  • W: Optics up Shift+W: Minimum impulse controller, pitch down ...
    3 KB (463 words) - 19:10, 11 May 2022
  • The '''[[w:Apollo_Lunar_Module|Lunar Module (LM)]]''' was the lander portion of the Ap ...
    1 KB (154 words) - 15:53, 17 April 2008
  • '''[[w:Apollo 15|Apollo 15]]''' was the ninth manned mission in the Apollo program ...
    1 KB (162 words) - 13:58, 19 October 2007
  • ...I]] is a kind of "artificial horizon", which is implemented by using the [[w:OpenGL|OpenGL]] interface. That can cause problems or even crashes with som ...lation"). Now you control the RHC with the joystick and the THC with the [[w:numeric keypad|numeric keypad]], a good alternative to two joysticks. ...
    8 KB (1,204 words) - 16:10, 30 July 2008
  • ...is [[w:Hypergolic_fuel|hypergolic fuel combination]] is pressurized with [[w:Helium|helium]] during thrusting periods, so no propellant pump is needed. ...
    8 KB (1,278 words) - 19:40, 31 May 2011
  • :'''''2''''' C/W POWER - 1 (UP) :'''''2''''' C/W - ACK (DOWN) ...
    10 KB (1,835 words) - 22:26, 18 February 2009
  • ...ter like" than the real Apollo spacecraft. The [[Simple AGC]] is used as [[w:Apollo_Guidance_Computer|Apollo Guidance Computer (AGC)]]. ...for the advanced users, who already have some basic knowledge about the [[w:Project_Apollo|Apollo missions]], are familiar with Orbiter and now want to ...
    6 KB (854 words) - 18:33, 14 January 2023
  • ...also not all joysticks have a yaw axis. Because of this additionally the [[w:joystick|POV "Hat" Switch]] can be used: ...
    3 KB (522 words) - 00:05, 31 July 2008
  • ...board Assembly''' (DSKY) was the main interface between the crew and the [[w:Apollo Guidance Computer | Apollo Guidance Computers]] which controlled the ...electroluminescence|electroluminescent display]] arranged in an array of [[w:seven segment display|seven segments]] per numeral, which is used to show i ...
    6 KB (1,109 words) - 22:00, 25 November 2006
  • ...e IMU platform with respect to the Basic Reference System by storing the [[w:Refsmmat|Reference to Stable Member Matrix (REFSMMAT)]] in it's erasable me | W ...
    11 KB (1,442 words) - 05:03, 21 March 2008
  • ...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