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(Q115871251)
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STAR 31
American solid rocket motor and stage developed by Thiokol
Antares 3
Antares III
STAR 31 Antares III
TE-M-762
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Statements
instance of
engine model
0 references
rocket model
0 references
subclass of
STAR
0 references
rocket stage
0 references
inception
1973
1 reference
reference URL
https://www.northropgrumman.com/wp-content/uploads/NG-Propulsion-Products-Catalog.pdf
page(s)
63
mass
1,384
kilogram
criterion used
launch weight
1 reference
reference URL
http://www.astronautix.com/a/antares3.html
98
kilogram
criterion used
dry weight
1 reference
reference URL
http://www.astronautix.com/a/antares3.html
follows
STAR 30
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followed by
STAR 37
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country of origin
United States of America
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diameter
0.7645
metre
1 reference
reference URL
https://www.northropgrumman.com/wp-content/uploads/NG-Propulsion-Products-Catalog.pdf
page(s)
63
source of energy
solid rocket propellant
has part(s)
ammonium perchlorate composite propellant
1 reference
reference URL
http://www.astronautix.com/a/antares3.html
maximum thrust
80.0
kilonewton
1 reference
reference URL
http://www.astronautix.com/a/antares3.html
specific impulse by weight
294
second
1 reference
reference URL
http://www.astronautix.com/a/antares3.html
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