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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]] ...

The CSM pyros are detonated by special pyro batteries, which are not connected to t ...9730011151_1973011151.pdf Apollo Experience Report: Spacecraft Pyrotechnic Systems] ...

...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 ...

...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 ...

...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)| ]] ...

'''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 ...

[[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. ...

...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? == ...

...ic failures in the simulation, generic switch failures are supported where systems see the state of a switch in a failed switch position, different from the a ...ion time (failure condition 1) since the start of the simulation. Only the CSM currently supports more failure conditions. ...

[[Category:CSM systems]] ...

[[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 ...

=== 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 ...

For the CSM this screen contains two parameters: *Status of CSM O2 Hose ...

[[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. ...

[[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] ...

...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]] ...

[[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 ...

...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 ...

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.]] ...

...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. ...

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. ...

[[Category:CSM systems]] [[Category:LM systems]] ...

...g for recent informations about the CSM panel, please use the [[CSM_panels|CSM panels]] article instead.}} <td>See also Apollo 15 CSM Launch Checklist</td> ...

...ta velocity (&Delta;V) manoevers during [[SPS]] or RCS thrusting along the CSM X-axis (foreward/backward). Both the SPS THRUST light and the &Delta;V nume ...be illuminated any time one of the SPS bipropellant engine injector valves systems A or B are open (powered) regardless which thrust mode is used, see the [[S ...

.../19730017161_1973017161.pdf Apollo experience report: Guidance and control systems - Digital autopilot design development] Since no listing is currently known to exist of CSM pad loads for any Collosus version, pad load variables and values had to be ...

...1976-1985 from modules launched using Saturn V INT-21s and modified Apollo CSM/LMs would carry astronauts from Earth to the base and back. ...s.nasa.gov/19640007807_1964007807.pdf Initial Concept Of Lunar Exploration Systems For Apollo. Volume I - Summary]'', March 1964 ...

...one or both of the two pairs of engine injector valves (bipropellant valve systems A or B) {{Panel label|name=3.D}} pneumatically. The gaseous nitrogen pressu ...rol of the SPS gimbal angles. The current attitude error is shown by the [[CSM FDAI|FDAI]] in the BMAG1 error display mode. To enable this mode for the pi ...

...posed Block-III CSM designed for extended orbital operations, the Block-IV CSM with batteries for power and LEM engines in place of the SPS and the Block- In addition, the inclusion of a Block-I CSM in future versions has been discussed. ...

...he quad's plumbing. Each RCS quad has its own individual fuel and plumbing systems. Each quad operates as its own independent system. For example, if quad A's [[Category:Reaction Control System (CSM)]] ...

...For the most part, you just ride along. In quickstart mode, there is no systems management that is required of you. However, there is much that is still a Now it's time to get in the LEM and head down to the surface. The CSM put you pretty close, so the LEM should have no problems actually getting y ...