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11D430
model of Soviet rocket engine
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instance of
product model
0 references
subclass of
rocket engine
0 references
country of origin
Soviet Union
0 references
manufacturer
A.M. Isayev Chemical Engineering Design Bureau
0 references
described by source
Encyclopedia Astronautica
subject named as
11D430
1 reference
reference URL
http://www.astronautix.com/1/11d430.html
retrieved
3 March 2022
source of energy
dinitrogen tetroxide
1 reference
reference URL
http://www.astronautix.com/1/11d430.html
1,1-dimethylhydrazine
1 reference
reference URL
http://www.astronautix.com/1/11d430.html
used by
Yantar-2K
1 reference
reference URL
http://www.astronautix.com/1/11d430.html
maximum thrust
29.43
kilonewton
1 reference
reference URL
http://www.astronautix.com/1/11d430.html
specific impulse by weight
307
second
1 reference
reference URL
http://www.astronautix.com/1/11d430.html
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11D430
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