Apollo 8 Mission Report(PDF). NASA. p. A-14. February 1969 [2013-06-28]. MSC-PA-R-69-1. (原始内容(PDF)存档于2013-03-02). 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公斤(33,278英磅), including propellants.
Apollo 8 Press Kit(PDF) (Press kit). NASA: 33–34. 1968-12-15 [2013-06-28]. Release No. 68-208. (原始内容存档(PDF)于2013-12-19). The spacecraft mass at launch includes the CM and SM, but excludes the 4,000公斤(8,900英磅) Launch Escape System (LES), which was discarded before reaching Earth orbit.
Apollo 8 Press Kit(PDF) (Press kit). NASA: 33–34. 1968-12-15 [2013-06-28]. Release No. 68-208. (原始内容存档(PDF)于2013-12-19). The spacecraft mass at launch includes the CM and SM, but excludes the 4,000公斤(8,900英磅) Launch Escape System (LES), which was discarded before reaching Earth orbit.
Apollo 8 Mission Report(PDF). NASA. p. A-14. February 1969 [2013-06-28]. MSC-PA-R-69-1. (原始内容(PDF)存档于2013-03-02). 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公斤(33,278英磅), including propellants.
Apollo 8 Mission Report(PDF). NASA: 3-2. February 1969 [2013-06-28]. MSC-PA-R-69-1. (原始内容存档(PDF)于2016-12-22).
Apollo 8 Mission Report(PDF). NASA. p. 3-1. February 1969 [2015-05-08]. MSC-PA-R-69-1. (原始内容存档(PDF)于2016-12-22).