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Hydac
American solid rocket motor
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Statements
subclass of
solid rocket booster
0 references
mass
253
kilogram
has characteristic
gross weight
1 reference
reference URL
http://www.astronautix.com/h/hydac.html
70
kilogram
has characteristic
zero-fuel weight
1 reference
reference URL
http://www.astronautix.com/h/hydac.html
based on
Javelin 3
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country of origin
United States of America
0 references
manufacturer
Lockheed Corporation
1 reference
reference URL
http://www.astronautix.com/h/hydac.html
service entry
1963
1 reference
reference URL
http://www.astronautix.com/h/hydac.html
service retirement
1988
1 reference
reference URL
http://www.astronautix.com/h/hydac.html
length
3.73
metre
1 reference
reference URL
http://www.astronautix.com/h/hydac.html
diameter
0.23
metre
1 reference
reference URL
http://www.astronautix.com/h/hydac.html
maximum thrust
45.5
kilonewton
1 reference
reference URL
http://www.astronautix.com/h/hydac.html
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