„Apollo 8 Mission Report”(PDF). NASA. februarie 1969. p. A-14. MSC-PA-R-69-1. Arhivat din original(PDF) la . Accesat în . The mass for LTA-B was less than that of a flying LM, because it was essentially a boilerplate descent stage. A fully loaded, flight-ready LM, like the Eagle from Apollo 11, had a mass of 15.095 kilograme (33.278lb), including propellants.
nssdc.gsfc.nasa.gov
„Apollo 8”. NASA Space Science Data Coordinated Archive. Arhivat din original la . Accesat în .
„Apollo 8 Press Kit”(PDF) (Press kit). NASA. . pp.33–34. Release No. 68-208. Accesat în . The spacecraft mass at launch includes the CM and SM, but excludes the 4.000 kilograme (8.900lb) Launch Escape System (LES), which was discarded before reaching Earth orbit.
„Apollo 8”. NASA Space Science Data Coordinated Archive. Arhivat din original la . Accesat în .
„Apollo 8 Mission Report”(PDF). NASA. februarie 1969. p. A-14. MSC-PA-R-69-1. Arhivat din original(PDF) la . Accesat în . The mass for LTA-B was less than that of a flying LM, because it was essentially a boilerplate descent stage. A fully loaded, flight-ready LM, like the Eagle from Apollo 11, had a mass of 15.095 kilograme (33.278lb), including propellants.
