"അപ്പോളോ 8" എന്ന താളിന്റെ പതിപ്പുകൾ തമ്മിലുള്ള വ്യത്യാസം

| launch_mass = CSM: {{convert|63650|lb|kg|order=flip}}<ref>{{cite web |url=http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19690003059_1969003059.pdf |title=Apollo 8 Press Kit |date=December 15, 1968 |publisher=NASA |pages=33–34 |type=Press kit |format=PDF |id=Release No. 68-208 |accessdate=June 28, 2013}} – The spacecraft mass at launch includes the CM and SM, but excludes the {{convert|8900|lb|kg|order=flip}} Launch Escape System (LES), which was discarded before reaching Earth orbit.</ref><br/>CM:{{convert|12392|lb|kg|order=flip}}<br/>SM:{{convert|51258|lb|kg|order=flip}}<br/>LTA: {{convert|19900|lb|kg|order=flip}}<ref>{{cite web |url=http://history.nasa.gov/ap08fj/pdf/a08-missionreport.pdf |title=Apollo 8 Mission Report |date=February 1969 |publisher=NASA |page=A-14 |format=PDF |id=MSC-PA-R-69-1 |accessdate=June 28, 2013 |archive-date=2013-03-02 |archive-url=https://web.archive.org/web/20130302223118/http://history.nasa.gov/ap08fj/pdf/a08-missionreport.pdf |url-status=dead }} – The mass for LTA-B was less than that of a flying LM, because it was essentially a boilerplate decent stage. A fully loaded, flight-ready LM, like the ''Eagle'' from Apollo 11, had a mass of {{convert|33278|lb|kg|order=flip}}, including propellants.</ref>