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UA1207
American solid rocket booster
Titan UA1207
UA-1207
Titan UA-1207
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Statements
instance of
rocket model
0 references
subclass of
UA1200
1 reference
reference URL
http://www.astronautix.com/u/ua1207.html
mass
319,330
kilogram
criterion used
gross weight
1 reference
reference URL
http://www.astronautix.com/u/ua1207.html
51,230
kilogram
criterion used
dry weight
1 reference
reference URL
http://www.astronautix.com/u/ua1207.html
country of origin
United States of America
1 reference
reference URL
http://www.astronautix.com/u/ua1207.html
manufacturer
Lockheed Martin
0 references
first flight
1989
1 reference
reference URL
http://www.astronautix.com/u/ua1207.html
height
34.14
metre
1 reference
reference URL
http://www.astronautix.com/u/ua1207.html
diameter
3.05
metre
1 reference
reference URL
http://www.astronautix.com/u/ua1207.html
described by source
Encyclopedia Astronautica
subject named as
UA1207
1 reference
reference URL
http://www.astronautix.com/u/ua1207.html
retrieved
20 September 2020
source of energy
polybutadiene acrylonitrile
1 reference
reference URL
http://www.astronautix.com/u/ua1207.html
used by
Titan IIIM
1 reference
reference URL
http://www.astronautix.com/u/ua1207.html
Titan IV
1 reference
reference URL
http://www.astronautix.com/u/ua1207.html
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Wikipedia
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UA1207
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