RD-0216
The RD-0216 and RD-0217 are liquid rocket engines, burning N2O4 and UDMH in the oxidizer rich staged combustion cycle. The only difference between the RD-0216 and the RD-0217 is that the latter has a heat exchanger to heat the pressuring gasses for the tanks. Three RD-0216 and one RD-0217 were used on the first stage of the UR-100 ICBM. The engines were manufactured until 1974 and stayed in operational use until 1991. More than 1100 engines were produced.
RD-0216
The RD-0216 and RD-0217 are liquid rocket engines, burning N2O4 and UDMH in the oxidizer rich staged combustion cycle. The only difference between the RD-0216 and the RD-0217 is that the latter has a heat exchanger to heat the pressuring gasses for the tanks. Three RD-0216 and one RD-0217 were used on the first stage of the UR-100 ICBM. The engines were manufactured until 1974 and stayed in operational use until 1991. More than 1100 engines were produced.
has abstract
RD-0216とRD-0217はN2O4とUDMHを酸化剤リ ...... 100NUとロコットとストレラ用のエンジンの製造は終了した。
@ja
The RD-0216 and RD-0217 are li ...... and Strela use it as of 2015.
@en
Link from a Wikipage to an external page
Wikipage page ID
47,021,696
Wikipage revision ID
741,589,511
associated
UR-100N, Rokot and Strela
combustion chamber
country of Origin
designer
first date
1965-04-19
1973-04-09
name
oxidiser
purpose
ICBM propulsion
status
successor
used in
UR-100 Core Stage
UR-100N Second Stage
subject
hypernym
type
comment
RD-0216とRD-0217はN2O4とUDMHを酸化剤リ ...... 100NUとロコットとストレラ用のエンジンの製造は終了した。
@ja
The RD-0216 and RD-0217 are li ...... an 1100 engines were produced.
@en
label
RD-0216
@en
RD-0216
@ja