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  • ...)]]''', providing a home and life support for the astronauts in space. The CSM consisted of two parts, the Command Module (CM) and the Service Module (SM) [[Image:CSM_in_Earth_orbit.jpg|thumb|right|The CSM in Earth orbit]] ...
    5 KB (787 words) - 21:36, 14 January 2017
  • The CSM pyros are detonated by special pyro batteries, which are not connected to t ...9730011151_1973011151.pdf Apollo Experience Report: Spacecraft Pyrotechnic Systems] ...
    2 KB (276 words) - 21:22, 29 November 2006
  • ...to get a better understanding and feeling how to work with the spacecraft systems. [[Image:CSM-CWS-Lights-Location.gif|thumb|right|450px|Location of Caution and Warning S ...
    4 KB (595 words) - 22:01, 21 October 2007
  • ...o-Soyuz test project. Operations handbook command/service/docking modules (CSM 119/DM 1): Operational procedures reference issue.'' July 15, 1974. [http:/ #A15_LAUNCH_CHECK ''Apollo 15 CSM Launch Checklist.'' July 9, 1971. NASA Manned Spacecraft Center. Houston, T ...
    5 KB (681 words) - 15:29, 10 March 2010
  • ...e Reaction Control System and Command Module Reaction Control System. Both systems are controlled either manually or automatically by the [[CMC]] or the [[SCS [[Category:Reaction Control System (CSM)| ]] ...
    2 KB (269 words) - 21:33, 7 June 2008
  • '''What changed:''' The value for specific heat used in the internal systems, fluids simulation, now uses separate specific heat values for gases and li ...l result in very high cryo pressures, and the internal temperature of some systems will change drastically. Generally it will be possible to conplete the miss ...
    2 KB (384 words) - 02:06, 14 September 2022
  • [[Image:CSM-Mission-Timer-Location.gif|thumb|250px|left|Location of Mission Timer contr ...s from the ground, but in Orbiter you can't have one person looking at the CSM panel while another looks at the LEM panel to activate the timer. ...
    3 KB (573 words) - 12:02, 3 December 2007
  • ...vessels than the real spacecraft and without the simulation of spacecraft systems or the Virtual AGC. There are already realistic panels, but only very few s == How can I separate the CSM or the CSM/LM stack from the SIVB? == ...
    4 KB (653 words) - 08:23, 1 October 2007
  • [[Category:CSM systems]] ...
    1 KB (188 words) - 02:45, 29 November 2006
  • [[Image:CSM_main_panel.jpg|thumb|right|CSM main control panel]] Most of the '''CSM Panel Controls and Displays''' are simulated as completely authentic, almos ...
    4 KB (675 words) - 14:12, 26 May 2009
  • === CSM main panel === The CSM 2D cockpit features fully functional control panels. Especially the CSM main panel is very large, which can cause frame rate problems with some gra ...
    8 KB (1,204 words) - 16:10, 30 July 2008
  • For the CSM this screen contains two parameters: *Status of CSM O2 Hose ...
    9 KB (1,605 words) - 15:57, 5 March 2022
  • [[Image:CSMECSDiagram.png|thumb|right|CSM Environmental Control System]] ...ou can use time acceleration up to 1000 to assure that all of the internal systems have reasonable reaction times. ...
    9 KB (1,529 words) - 23:56, 19 December 2006
  • [[Image:CSM-SECS-Controls.jpg|thumb|250px|right|SECS logic switches and circuit breaker ....gov/afj/aoh/aoh-v1-2-09-seqsys.pdf Apollo Operations Handbook: Sequential Systems] ...
    2 KB (302 words) - 18:27, 6 December 2006
  • ...te simulation of the Command Module control panel and most of the internal systems, and support for new spacecraft. It is also capable of flying most of an Ap [[Image:NASSP4_CSM_LM.jpg|thumb|left|NASSP 4 CSM & LM]] ...
    7 KB (1,162 words) - 13:09, 22 February 2017
  • [[Category:Reaction Control System (CSM)]] ...otion. The CM RCS contains only 12 rockets in two completely redundant sub-systems named system 1 and system 2. These 12 reaction control jets allow the comma ...
    6 KB (962 words) - 18:47, 13 May 2011
  • ...Electrical Power System (EPS) supplies electrical power to almost all CSM systems. ..., heat and water (H2O) are produced. Electricity is distributed to the CSM systems, the excess heat is radiated to space, water is distributed to the Environm ...
    17 KB (3,004 words) - 17:47, 19 February 2009
  • The '''[[IMU|Inertial Measurement Unit (IMU)]]''' is used to determine the [[CSM]] and [[LM]] attitude with respect to an inertial, star-fixed system. Indep [[Image:CSM Scanning Telescope.jpg|thumb|right|Navigation star 23 in the CSM Scanning Telescope.]] ...
    11 KB (1,442 words) - 05:03, 21 March 2008
  • ...h the displayed parameters, you should input them into either the AGC (the CSM [[AGC]] controls the burn) or the Project Apollo MFD (the [[w:Saturn_V_Inst * Ensure all RCS and engine gimbal systems are activated before T-1:30. ...
    6 KB (1,008 words) - 17:09, 27 September 2007
  • The '''Guidance and Control System''' consisted of a number of sub-systems for in-flight navigation and guidance. ...ub-systems: detailed information use will be on individual pages for those systems. ...
    19 KB (3,215 words) - 17:39, 26 May 2011
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