Reaction Control System (CSM) - Revision history

imported>Tschachim: clarification

2008-06-07T21:33:14Z

clarification

← Older revision		Revision as of 21:33, 7 June 2008
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	The Command Module Reaction Control System (CM RCS) provides the impulse required for controlling spacecraft rates and attitude during the terminal phase of the mission after SM separation.		The Command Module Reaction Control System (CM RCS) provides the impulse required for controlling spacecraft rates and attitude during the terminal phase of the mission after SM separation.

	The CM RCS consists of two similar and independent subsystems, identified as system 1 and system 2. The CM RCS is contained entirely within the CM and each reaction engine nozzle is ported through the CM skin. ~~The CM RCS uses the same propellants and pressurization as the SM RCS.~~		The CM RCS consists of two similar and independent subsystems, identified as system 1 and system 2. The CM RCS is contained entirely within the CM and each reaction engine nozzle is ported through the CM skin.

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imported>Tschachim: Done for now.

2008-06-07T20:22:51Z

Done for now.

← Older revision		Revision as of 20:22, 7 June 2008
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	{{mainarticle\|Service Module Reaction Control System}}		{{mainarticle\|Service Module Reaction Control System}}

			The Service Module Reaction Control System (SM RCS) consists of four individual, functionally identical packages, located 90° apart around the forward (+X axis) of the SM periphery. Each package, called a "quad", is such that the reaction engines are mounted on the outer surface of the panel and the remaining components are inside.

			Each RCS package incorporates a pressure-fed, positive-expulsion, pulse-modulated, bipropellant system to produce the reaction thrust required to perform the various SM RCS control functions.

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	== Command Module Reaction Control System ==		== Command Module Reaction Control System ==
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	{{mainarticle\|Command Module Reaction Control System}}		{{mainarticle\|Command Module Reaction Control System}}

			The Command Module Reaction Control System (CM RCS) provides the impulse required for controlling spacecraft rates and attitude during the terminal phase of the mission after SM separation.

			The CM RCS consists of two similar and independent subsystems, identified as system 1 and system 2. The CM RCS is contained entirely within the CM and each reaction engine nozzle is ported through the CM skin. The CM RCS uses the same propellants and pressurization as the SM RCS.

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	#[[References]]		#[[References]]
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	[[Category:Reaction Control System (CSM)\| ]]		[[Category:Reaction Control System (CSM)\| ]]


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imported>Tschachim: Work in progress...

2008-06-06T23:52:04Z

Work in progress...

← Older revision		Revision as of 23:52, 6 June 2008
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	== ~~Command~~ Module Reaction Control System ==		The '''Reaction Control System (RCS)''' provides the thrust to control spacecraft rates and rotation in all three axis in addition to any minor translation maneuvers. The [[CSM]] includes two separate reaction control systems designated Service Module Reaction Control System and Command Module Reaction Control System. Both systems are controlled either manually or automatically by the [[CMC]] or the [[SCS]].

			== Service Module Reaction Control System ==

	[[Image:~~CM_RCS_diagram~~.jpg\|thumb\|right\|The ~~Command~~ Module Reaction Control System<cite>AOH</cite>]]		[[Image:SM_RCS_diagram.jpg\|thumb\|right\|The Service Module Reaction Control System<cite>AOH</cite>]]

	{{mainarticle\|~~Command~~ Module Reaction Control System}}		{{mainarticle\|Service Module Reaction Control System}}

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	~~== Service Module Reaction Control System ==~~

	[[Image:~~SM_RCS_diagram~~.jpg\|thumb\|right\|The ~~Service~~ Module Reaction Control System<cite>AOH</cite>]]		== Command Module Reaction Control System ==

			[[Image:CM_RCS_diagram.jpg\|thumb\|right\|The Command Module Reaction Control System<cite>AOH</cite>]]

	{{mainarticle\|~~Service~~ Module Reaction Control System}}		{{mainarticle\|Command Module Reaction Control System}}

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imported>Tschachim: headings

2008-06-06T23:26:00Z

headings

← Older revision		Revision as of 23:26, 6 June 2008
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			== Command Module Reaction Control System ==

			[[Image:CM_RCS_diagram.jpg\|thumb\|right\|The Command Module Reaction Control System<cite>AOH</cite>]]

			{{mainarticle\|Command Module Reaction Control System}}

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			== Service Module Reaction Control System ==

			[[Image:SM_RCS_diagram.jpg\|thumb\|right\|The Service Module Reaction Control System<cite>AOH</cite>]]

			{{mainarticle\|Service Module Reaction Control System}}

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			<biblio force=false>
			#[[References]]
			</biblio>



	[[Category:Reaction Control System (CSM)\| ]]		[[Category:Reaction Control System (CSM)\| ]]

imported>Tschachim: stub

2008-06-06T18:06:59Z

stub

New page

[[Category:Reaction Control System (CSM)| ]]

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