Jump to content

RD-0236: Difference between revisions

From Wikipedia, the free encyclopedia
Browse history interactively
← Previous edit
Content deleted Content added
VisualWikitext
m →References: multiple columns for better legibility.
Darkcoucou (talk | contribs)
341 edits
Repaired several Dead Sources by providing Webarchive Source
 
(7 intermediate revisions by 5 users not shown)
Line 52: Line 52:
|notes =
|notes =
}}
}}
The '''RD-0236''' ([[GRAU]] Index '''15D114''') is a [[liquid-fuel rocket|liquid]] [[rocket engine|rocket]] [[Vernier thruster|vernier engine]], burning [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]] and [[Unsymmetrical dimethylhydrazine|UDMH]] in the [[Gas-generator cycle (rocket)|gas generator]] cycle.<ref name=khrun-rockot /><ref name=kbkha-rd0233 /> It is used along the [[RD-0235]] main engine on the [[UR-100N|UR-100UTTKh]] second stage. Its function is to supply [[Thrust vectoring|thrust vector control]] by [[Gimbaled thrust|gimbaling]] each of its four nozzles in a plane.<ref name=ea-rd0236 /> While the engine is out of production, the [[UR-100N|ICBM]] as well as [[Rokot]] and [[Strela (rocket)|Strela]] remain operational as of 2015.<ref name=rsw-ur100n />
The '''RD-0236''' ([[GRAU]] Index '''15D114''') is a [[liquid-fuel rocket|liquid]] [[rocket engine|rocket]] [[Vernier thruster|vernier engine]], burning [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]] and [[Unsymmetrical dimethylhydrazine|UDMH]] in the [[Gas-generator cycle (rocket)|gas generator]] cycle.<ref name=khrun-rockot /><ref name=kbkha-rd0233 /> It is used along the [[RD-0235]] main engine on the UTTKh second stage, which was featured in the [[UR-100N]] ICBM as well as the [[Strela (rocket)|Strela]] and [[Rokot]] launch vehicles derived from it. Its function is to supply [[Thrust vectoring|thrust vector control]] by [[Gimbaled thrust|gimbaling]] each of its four nozzles in a plane.<ref name=ea-rd0236 /> While the engine is out of production, the [[UR-100N|ICBM]] as well as [[Strela (rocket)|Strela]] remain operational as of 2015.<ref name=rsw-ur100n /> The [[Rokot]] launch vehicle conducted its final launch before retirement in December 2019.<ref>{{Cite web|url=https://www.nasaspaceflight.com/2019/12/rokot-final-launch-three-gonets-m-satellites/|title=Rokot conducts final launch – carries three Gonets-M satellites to orbit|date=2019-12-26|access-date=2020-03-06|website=[[NASASpaceFlight.com]]|last=Graham|first=William}}</ref>


==See also==
==See also==
Line 63: Line 63:
== References ==
== References ==
{{reflist|30em|refs=
{{reflist|30em|refs=
<ref name=kbkha-rd0233>{{cite web |url=http://www.kbkha.ru/?p=8&cat=10&prod=47 |title= RD-0233, RD-0234, RD-0235, RD-0236, RD-0237. Intercontinental ballistic missiles RS-18 |publisher=KBKhA |accessdate=2015-06-19}}</ref>
<ref name=kbkha-rd0233>{{cite web |url=http://www.kbkha.ru/?p=8&cat=10&prod=47 |title= RD-0233, RD-0234, RD-0235, RD-0236, RD-0237. Intercontinental ballistic missiles RS-18 |publisher=KBKhA |url-status=dead |archive-url=https://web.archive.org/web/20140505124803/http://www.kbkha.ru/?p=8&cat=10&prod=47 |archive-date=5 May 2014}}</ref>
<ref name=khrun-rockot>{{cite web |url=http://www.khrunichev.ru/main.php?id=43 |title= Rockot Launch Vehicle |publisher=[[Khrunichev|Khrunichev State Research and Production Space Center]] |accessdate=2015-06-19}}</ref>
<ref name=khrun-rockot>{{cite web |url=http://www.khrunichev.ru/main.php?id=43 |title= Rockot Launch Vehicle |publisher=[[Khrunichev|Khrunichev State Research and Production Space Center]] |url-status=dead |archive-url=https://web.archive.org/web/20110527161252/http://www.khrunichev.ru/main.php?id=43 |archive-date=27 May 2011}}</ref>
<ref name=ea-rd0236>{{cite web |url=http://www.astronautix.com/engines/rd0236.htm |title=RD-0236 |website=Encyclopedia Astronautica |accessdate=2015-06-19}}</ref>
<ref name=ea-rd0236>{{cite web |url=http://www.astronautix.com/engines/rd0236.htm |archive-url=https://web.archive.org/web/20020505192948/http://www.astronautix.com/engines/rd0236.htm |url-status=dead |archive-date=May 5, 2002 |title=RD-0236 |website=Encyclopedia Astronautica |access-date=2015-06-19}}</ref>
<ref name=rsw-ur100n>{{cite web |url=http://www.russianspaceweb.com/ur100n.html |title=UR-100N Family |last=Zak |first=Anatoly |website=RussianSpaceWeb.com |accessdate=2015-06-19}}</ref>
<ref name=rsw-ur100n>{{cite web |url=http://www.russianspaceweb.com/ur100n.html |title=UR-100N Family |last=Zak |first=Anatoly |website=RussianSpaceWeb.com |access-date=2015-06-19}}</ref>
}}
}}


== External links ==
== External links ==
* [http://www.kbkha.ru/?p=8&cat=10&prod=47 KbKhA official information on the engine.]
* [https://web.archive.org/web/20140505124803/http://www.kbkha.ru/?p=8&cat=10&prod=47 KbKhA official information on the engine. ''(Archived)'']
* [http://www.astronautix.com/engines/rd0233.htm Encyclopedia Astronautica information on the propulsion module.]
* [https://web.archive.org/web/20150824113748/http://www.astronautix.com/engines/rd0233.htm Encyclopedia Astronautica information on the propulsion module. ''(Archived)'']

⚫
{{Rocket engines}}


⚫
{{Rocket Engines}}
[[Category:Spaceflight]]
⚫
[[Category:Rocket engines]]
[[Category:Rocket engines of the Soviet Union]]
[[Category:Rocket engines of the Soviet Union]]
[[Category:Rocket engines using hypergolic propellant]]
[[Category:Rocket engines using hypergolic propellant]]
[[Category:Rocket engines using the gas-generator cycle]]
⚫
[[Category:KBKhA rocket engines]]


{{rocket-stub}}
{{rocket-stub}}

Latest revision as of 10:27, 24 July 2022

RD-0236 (РД-0236)
Country of originUSSR
First flight1973-04-09[1]
DesignerOKB-154[1]
ApplicationVernier engine
Associated LVUR-100N, Rokot and Strela[1]
StatusOut of Production
Liquid-fuel engine
PropellantN2O4[1] / UDMH[1]
CycleGas Generator[1]
Configuration
Chamber4[2]
Performance
Thrust15.76 kilonewtons (3,540 lbf)[2]
Specific impulse, vacuum293 s (2.87 km/s)[2]
Used in
UR-100N second stage[2]

The RD-0236 (GRAU Index 15D114) is a liquid rocket vernier engine, burning N2O4 and UDMH in the gas generator cycle.[3][1] It is used along the RD-0235 main engine on the UTTKh second stage, which was featured in the UR-100N ICBM as well as the Strela and Rokot launch vehicles derived from it. Its function is to supply thrust vector control by gimbaling each of its four nozzles in a plane.[2] While the engine is out of production, the ICBM as well as Strela remain operational as of 2015.[4] The Rokot launch vehicle conducted its final launch before retirement in December 2019.[5]

See also

[edit]

References

[edit]
  1. ^ a b c d e f g "RD-0233, RD-0234, RD-0235, RD-0236, RD-0237. Intercontinental ballistic missiles RS-18". KBKhA. Archived from the original on 5 May 2014.
  2. ^ a b c d e "RD-0236". Encyclopedia Astronautica. Archived from the original on May 5, 2002. Retrieved 2015-06-19.
  3. ^ "Rockot Launch Vehicle". Khrunichev State Research and Production Space Center. Archived from the original on 27 May 2011.
  4. ^ Zak, Anatoly. "UR-100N Family". RussianSpaceWeb.com. Retrieved 2015-06-19.
  5. ^ Graham, William (2019-12-26). "Rokot conducts final launch – carries three Gonets-M satellites to orbit". NASASpaceFlight.com. Retrieved 2020-03-06.
[edit]
Stub icon

This rocketry article is a stub. You can help Wikipedia by expanding it.

Retrieved from "https://en.wikipedia.org/enwiki/w/index.php?title=RD-0236&oldid=1100133931"