|lunar_module = '''Ballast:''' LM Test Article B<br />{{convertরূপান্তর|19900|lb|kg|abbr=on}}<ref>{{সাময়িকী উদ্ধৃতি | authorলেখক = Mission Evaluation Team | titleশিরোনাম = Appendix A: A.5 Lunar Module Test Article | journalসাময়িকী = Apollo 8 Mission Report | pageপাতা = p. A-14 | yearবছর = 1969 | month = February | urlইউআরএল = http://history.nasa.gov/ap08fj/pdf/a08-missionreport.pdf | postscriptপুনশ্চ = <!--None--> }} – 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'', weighed {{convertরূপান্তর|33278|lb|kg|abbr=on}}, including propellants.</ref>
| authorলেখক = NASA Public Affairs Office | titleশিরোনাম = SPACECRAFT STRUCTURE SYSTEMS | journalসাময়িকী = Apollo 8 Press Kit | pagesপাতাসমূহ = pp. 33–34 | dateতারিখ = 1968-12-06 | urlইউআরএল = http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19690003059_1969003059.pdf
| postscriptপুনশ্চ = <!--None--> }} – The spacecraft mass at launch includes the CM and SM, but excludes the {{convertরূপান্তর|8900|lb|kg|adj=on}} Launch Escape System (LES), which was discarded before reaching Earth orbit.</ref><br />CM:{{convertরূপান্তর|12392|lb|kg|abbr=on}}<br />SM:{{convertরূপান্তর|51258|lb|kg|abbr=on}}
|booster = [[শনি ৫]] এস.এ. ৫০৩
|crew_size = ৩
|launch_pad = [[Kennedy Space Center Launch Complex 39|LC 39A]], {{nowrap|[[Kennedy Space Center]]}}<br />ফ্লোরিডা, যুক্তরাষ্ট্র
