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Fregat-M
model of Russian rocket upper stage
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Statements
instance of
rocket model
0 references
subclass of
Fregat
0 references
mass
980
kilogram
criterion used
dry weight
1 reference
reference URL
http://www.laspace.ru/rus/fregat_construction.php
archive URL
https://web.archive.org/web/20151226122333/http://www.laspace.ru/rus/fregat_construction.php
6,580
kilogram
criterion used
launch weight
1 reference
reference URL
http://www.laspace.ru/rus/fregat_construction.php
archive URL
https://web.archive.org/web/20151226122333/http://www.laspace.ru/rus/fregat_construction.php
country of origin
Russia
1 reference
reference URL
https://space.skyrocket.de/doc_stage/fregat.htm
manufacturer
NPO Lavochkin
1 reference
reference URL
https://www.russianspaceweb.com/fregat.html
powered by
S5.92
quantity
1
source of energy
1,1-dimethylhydrazine
hydrazine
1 reference
reference URL
https://space.skyrocket.de/doc_stage/fregat.htm
reaction control system
quantity
12
source of energy
hydrazine
0 references
developer
NPO Lavochkin
1 reference
reference URL
https://www.russianspaceweb.com/fregat.html
height
1.55
metre
1 reference
reference URL
http://www.laspace.ru/rus/fregat_construction.php
archive URL
https://web.archive.org/web/20151226122333/http://www.laspace.ru/rus/fregat_construction.php
diameter
3.35
metre
1 reference
reference URL
http://www.laspace.ru/rus/fregat_construction.php
archive URL
https://web.archive.org/web/20151226122333/http://www.laspace.ru/rus/fregat_construction.php
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