File:Translunar Coast Abort Modes - Lunar Landing Symposium, MSC Jun66.jpg

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Description	English: During the Trans-Lunar Coast phase of an Apollo lunar landing mission, four abort modes are specified, with different thrust options. The Service Propulsion System (SPS) engine is identified as primary, with the Lunar Module Descent Propulsion System (LM DPS) being available as optional or backup. The much weaker Service Module Reaction Control System (SM RCS) is available with only marginal capability on all modes but the Direct Abort. See text at [1]
Date	June 1966
Source	APOLLO LUNAR LANDING MISSION SYMPOSIUM - JUNE 25-27, 1966 MSC - VOLUME II - APOLLO EARTH RETURN ABORT CAPABILITIES
Author	Ronald L. Berry

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	Date/Time	Thumbnail	Dimensions	User	Comment
current	22:05, 8 July 2014		1,248 × 992 (154 KB)	Ras67 (talk \| contribs)	losslessly cropped with Jpegcrop
	09:16, 15 March 2010		1,280 × 1,024 (171 KB)	Tdadamemd (talk \| contribs)	{{Information \|Description={{en\|1=During the Trans-Lunar Coast phase of an Apollo lunar landing mission, four abort modes are specified, with different thrust options. The Service Propulsion System (SPS) engine is identified as primary, with the Lunar Mod

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