„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 (33.278 lb), including propellants.
nssdc.gsfc.nasa.gov
„Apollo 8”. NASA Space Science Data Coordinated Archive. 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 (8.900 lb) Launch Escape System (LES), which was discarded before reaching Earth orbit.
„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 (33.278 lb), including propellants.
