About: VS-40 (Foguete Suborbital VS-40)

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The VS-40 (Foguete Suborbital VS-40) is a Brazilian sounding rocket using solid fuel, stabilized aerodynamically, distributed between the first stage S40TM (4,200 kg) engine and the second stage S44M (810 kg) engine.This configuration corresponds to the upper stages of the VLS-1 rocket.

Attributes	Values
rdfs:comment	The VS-40 (Foguete Suborbital VS-40) is a Brazilian sounding rocket using solid fuel, stabilized aerodynamically, distributed between the first stage S40TM (4,200 kg) engine and the second stage S44M (810 kg) engine.This configuration corresponds to the upper stages of the VLS-1 rocket.
foaf:name	VS-40 (Foguete Suborbital VS-40)
foaf:depiction
country origin	Brazil
diameter (μ)	1(xsd:double)
failed launches	0(xsd:integer)
height (μ)	9(xsd:double)
launch site	Alcântara Launch Center dbpedia:Andøya_Space_Center Barreira do Inferno Launch Center
lower earth orbit payload (g)	500000(xsd:double)
maiden flight	1993-04-02(xsd:dateTime)
manufacturer	dbpedia:Instituto_de_Aeronáutica_e_Espaço
mass (g)	6800000(xsd:double)
rocket function	dbpedia:Sounding_rocket
number of rocket stages	2(xsd:integer)
status	Active
thumbnail	http://commons.wikimedia.org/wiki/Special:FilePath/Foguete_VS_40.jpg?width=300
total launches	3(xsd:integer)

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