BOR-5

The BOR-5 is a 1:8 sized test flight vehicle, used to study the main aerodynamic, thermal, acoustic and stability characteristics of the Buran. It follows upon the BOR-4 reentry test vehicle.

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1984  Wikimedia, Wikidata
mass 1450 kilogram, 
sub-orbital spaceplane, test article, NPO Molniya, Soviet Union, 
Ashkenaz, Calvinist Republic of Ghent, Chinland, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Reman, Sikh Confederacy, Tarshish, Dong Fang Hong 2, Ekran, sub-orbital spaceplane, 1984, Republic of Haiti, 1980s, 

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Location: KML, Cluster Map, Maps,

1984-06-05T00:00:00Z

1984-06-05T00:00:00Z

1984 BOR-5

1986-12-27T00:00:00Z

1986-12-27T00:00:00Z

rocket launch

1984-07-05T00:00:00Z

1984-07-05T00:00:00Z

rocket launch

1985-04-17T00:00:00Z

1985-04-17T00:00:00Z

rocket launch

1987-08-27T00:00:00Z

1987-08-27T00:00:00Z

rocket launch

1988-06-21T00:00:00Z

1988-06-21T00:00:00Z

rocket launch

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Frameless

Type	Subtype	Date	Description	Notes	Source