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Apollo 8 (Malay Wikipedia)

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

refsWebsite
Global rank Malay rank
5nasa.gov
75th place
87th place
2web.archive.org
1st place
1st place
2wikipedia.org
low place
low place
1guardian.co.uk
197th place
248th place

guardian.co.uk (Global: 197th place; Malay: 248th place)

nasa.gov (Global: 75th place; Malay: 87th place)

history.nasa.gov

  • 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.

ntrs.nasa.gov

  • 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.

hq.nasa.gov

nasa.gov

web.archive.org (Global: 1st place; Malay: 1st place)

  • 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.

wikipedia.org (Global: low place; Malay: low place)

en.wikipedia.org

  • 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.