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Node 4 would have been built using the Node Structural Test Article (STA) and docked to the forward port of the [[Harmony (ISS module)|''Harmony'' module]]. The Structural Test Article was built to facilitate testing of ISS hardware and was intended to become Node 1. However, during construction, structural design flaws were discovered. The under-construction Node 2 was renamed Node 1 and the STA (ex-Node 1) was put into storage at the Kennedy Space Center (KSC).<ref>{{cite web |url=http://www.spaceref.com/iss/elements/node2.html |title=Space Station User's Guide |publisher=SpaceRef |access-date=2013-11-22 |archive-date=2012-12-16 |archive-url=https://archive.today/20121216130522/http://www.spaceref.com/iss/elements/node2.html |url-status=dead }}</ref>

Node 4 would have been built using the Node Structural Test Article (STA) and docked to the forward port of the [[Harmony (ISS module)|''Harmony'' module]]. The Structural Test Article was built to facilitate testing of ISS hardware and was intended to become Node 1. However, during construction, structural design flaws were discovered. The under-construction Node 2 was renamed Node 1 and the STA (ex-Node 1) was put into storage at the Kennedy Space Center (KSC).<ref>{{cite web |url=http://www.spaceref.com/iss/elements/node2.html |title=Space Station User's Guide |publisher=SpaceRef |access-date=2013-11-22 |archive-date=2012-12-16 |archive-url=https://archive.today/20121216130522/http://www.spaceref.com/iss/elements/node2.html |url-status=dead }}</ref>



Since the [[Space Shuttle program]] was retired, had a decision to build and launch Node 4 been taken, it would have been launched by an [[Atlas V]] or [[Delta IV]] rocket.<ref name="NasaSpaceflight" />

Since the [[Space Shuttle program]] was retired, had a decision to build and launch Node 4 be taken, it would have been launched by an [[Atlas V]] or [[Delta IV]] rocket.<ref name="NasaSpaceflight" />



In December 2011 [[Boeing]] proposed using Node 4 as the core of an [[Exploration Gateway Platform]] to be constructed at the [[ISS]] and relocated via [[space tug]] to an Earth-Moon [[Lagrange point]] (EML-1 or 2). The purpose of the platform would be to support lunar landing missions with a reusable [[Apollo Lunar Module|lunar lander]] after the first two [[Space Launch System|SLS]] flights. It would also satisfy the need for a L1 [[propellant depot]] for lunar missions. Other hardware would include an airlock, an 'international module', and a [[MPLM]] based habitat module.<ref>{{cite web|author=Chris Bergin |url=http://www.nasaspaceflight.com/2011/12/exploration-gateway-platform-hosting-reusable-lunar-lander-proposed/ |title=Exploration Gateway Platform hosting Reusable Lunar Lander proposed |publisher=NASASpaceFlight.com |date=2011-12-02 |access-date=2013-11-22}}</ref>

In December 2011 [[Boeing]] proposed using Node 4 as the core of an [[Exploration Gateway Platform]] to be constructed at the [[ISS]] and relocated via [[space tug]] to an Earth-Moon [[Lagrange point]] (EML-1 or 2). The purpose of the platform would be to support lunar landing missions with a reusable [[Apollo Lunar Module|lunar lander]] after the first two [[Space Launch System|SLS]] flights. It would also satisfy the need for a L1 [[propellant depot]] for lunar missions. Other hardware would include an airlock, an 'international module', and a [[MPLM]] based habitat module.<ref>{{cite web|author=Chris Bergin |url=http://www.nasaspaceflight.com/2011/12/exploration-gateway-platform-hosting-reusable-lunar-lander-proposed/ |title=Exploration Gateway Platform hosting Reusable Lunar Lander proposed |publisher=NASASpaceFlight.com |date=2011-12-02 |access-date=2013-11-22}}</ref>

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Greek: Ά ά Έ έ Ή ή Ί ί Ό ό Ύ ύ Ώ ώ   Α α Β β Γ γ Δ δ   Ε ε Ζ ζ Η η Θ θ   Ι ι Κ κ Λ λ Μ μ   Ν ν Ξ ξ Ο ο Π π   Ρ ρ Σ σ ς Τ τ Υ υ   Φ φ Χ χ Ψ ψ Ω ω   {{Polytonic|}}
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