Apollo 8 (Malay Wikipedia)

Analysis of information sources in references of the Wikipedia article "Apollo 8" in Malay language version.

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guardian.co.uk

Mission Evaluation Team (1969). "Appendix A: A.5 Lunar Module Test Article" (PDF). Apollo 8 Mission Report: p. A-14. Diarkibkan daripada yang asal (PDF) pada 2013-03-02. Dicapai pada 2012-12-22. Unknown parameter |month= ignored (bantuan); |page= has extra text (bantuan) – 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 33,278 lb (15,095 kg), including propellants.
"Apollo Flight Journal, Day 8". NASA. Diarkibkan daripada yang asal pada 2007-10-02. Dicapai pada 2012-12-22.

NASA Public Affairs Office (1968-12-06). "SPACECRAFT STRUCTURE SYSTEMS" (PDF). Apollo 8 Press Kit: pp. 33–34. |pages= has extra text (bantuan) – The spacecraft mass at launch includes the CM and SM, but excludes the 8,900-paun (4,000 kg) Launch Escape System (LES), which was discarded before reaching Earth orbit.

Mission Evaluation Team (1969). "Appendix A: A.5 Lunar Module Test Article" (PDF). Apollo 8 Mission Report: p. A-14. Diarkibkan daripada yang asal (PDF) pada 2013-03-02. Dicapai pada 2012-12-22. Unknown parameter |month= ignored (bantuan); |page= has extra text (bantuan) – 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 33,278 lb (15,095 kg), including propellants.
"Apollo Flight Journal, Day 8". NASA. Diarkibkan daripada yang asal pada 2007-10-02. Dicapai pada 2012-12-22.

Mission Evaluation Team (1969). "Appendix A: A.5 Lunar Module Test Article" (PDF). Apollo 8 Mission Report: p. A-14. Diarkibkan daripada yang asal (PDF) pada 2013-03-02. Dicapai pada 2012-12-22. Unknown parameter |month= ignored (bantuan); |page= has extra text (bantuan) – 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 33,278 lb (15,095 kg), including propellants.
NASA Public Affairs Office (1968-12-06). "SPACECRAFT STRUCTURE SYSTEMS" (PDF). Apollo 8 Press Kit: pp. 33–34. |pages= has extra text (bantuan) – The spacecraft mass at launch includes the CM and SM, but excludes the 8,900-paun (4,000 kg) Launch Escape System (LES), which was discarded before reaching Earth orbit.