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Sputnik 8A91
Soviet Union space launch vehicle
8A91
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Statements
instance of
rocket model
0 references
subclass of
expendable launch vehicle
0 references
liquid-propellant rocket
0 references
mass
269,300
kilogram
criterion used
gross weight
1 reference
reference URL
http://astronautix.com/s/sputnik8a91.html
based on
R-7 Semyorka
0 references
country of origin
Soviet Union
0 references
manufacturer
NPO Energomash
1 reference
reference URL
http://astronautix.com/s/sputnik8a91.html
first flight
27 April 1958
1 reference
reference URL
http://astronautix.com/s/sputnik8a91.html
payload mass
1,327
kilogram
1 reference
reference URL
http://astronautix.com/s/sputnik8a91.html
total produced
2
1 reference
reference URL
http://astronautix.com/s/sputnik8a91.html
service retirement
15 May 1958
1 reference
reference URL
http://astronautix.com/s/sputnik8a91.html
width
9.76
metre
1 reference
reference URL
http://astronautix.com/s/sputnik8a91.html
height
31.1
metre
1 reference
reference URL
http://astronautix.com/s/sputnik8a91.html
maximum thrust
3,784.9
kilonewton
1 reference
reference URL
http://astronautix.com/s/sputnik8a91.html
has part(s) of the class
Sputnik 8A91-0
quantity
4
0 references
Sputnik 8A91-1
quantity
1
0 references
Sitelinks
Wikipedia
(2 entries)
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glwiki
Sputnik 8A91
plwiki
Sputnik 8A91
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Wikiquote
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Wikiversity
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Wikivoyage
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Wiktionary
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Multilingual sites
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