RD-250
The RD-250 (GRAU Index 8D518) is the base version of a dual nozzle family of liquid rocket engines, burning N2O4 and UDMH in the oxidizer rich staged combustion cycle. The RD-250 was developed by OKB-456 for Yangel's PA Yuzhmash ICBM, the R-36 (missile) (8K67). Its variations were also used on the Tsyklon-2 and Tsyklon-3 launch vehicles. It was supposed to be used on the Tsyklon-4, but since the cancellation of the project it should be considered as out of production.
RD-250
The RD-250 (GRAU Index 8D518) is the base version of a dual nozzle family of liquid rocket engines, burning N2O4 and UDMH in the oxidizer rich staged combustion cycle. The RD-250 was developed by OKB-456 for Yangel's PA Yuzhmash ICBM, the R-36 (missile) (8K67). Its variations were also used on the Tsyklon-2 and Tsyklon-3 launch vehicles. It was supposed to be used on the Tsyklon-4, but since the cancellation of the project it should be considered as out of production.
has abstract
The RD-250 (GRAU Index 8D518) ...... nsidered as out of production.
@en
Link from a Wikipage to an external page
Wikipage page ID
50,995,215
Wikipage revision ID
741,589,635
associated
R-36, Tsyklon-2 and Tsyklon-3
combustion chamber
country of Origin
designer
first date
1965-12-16
manufacturer
mixture ratio
oxidiser
status
Out of Production
used in
R-36, Tsyklon-2 and Tsyklon-3 first stage
subject
comment
The RD-250 (GRAU Index 8D518) ...... nsidered as out of production.
@en
label
RD-250
@en