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|type =liquid
|type =liquid
|oxidiser =[[LOX]]
|oxidiser =[[LOX]]
|fuel =[[RG-1 (propellant)|RG-1]]
|fuel =[[RP-1]]
|mixture_ratio =2.65
|mixture_ratio =2.65
|cycle =[[Staged combustion cycle (rocket)|Staged Combustion]]
|cycle =[[Staged combustion cycle (rocket)|Staged Combustion]]
Line 66: Line 66:
==References==
==References==
{{Reflist|30em|refs=
{{Reflist|30em|refs=
<ref name=b14643-ukrainepropulsion>{{cite web |url=http://www.b14643.de/Spacerockets/Diverse/Ukrainian_Rocket_engines/engines.htm |title=Ukrainian space-rocket and missile liquid-propellant engines |first=Norbert |last=Brügge |publisher=B14643.de |date=2016-07-11 |accessdate=2015-08-06 }}{{dead link|date=April 2018 |bot=InternetArchiveBot |fix-attempted=yes }}</ref>
<ref name=b14643-ukrainepropulsion>{{cite web |url=http://www.b14643.de/Spacerockets/Diverse/Ukrainian_Rocket_engines/engines.htm |title=Ukrainian space-rocket and missile liquid-propellant engines |first=Norbert |last=Brügge |publisher=B14643.de |date=2016-07-11 |access-date=2015-08-06 }}{{dead link|date=April 2018 |bot=InternetArchiveBot |fix-attempted=yes }}</ref>
<ref name=khai-aktt201301p4450>{{cite journal |last1=Degtyarev |first1=A . V. |last2=Shulga |first2=V . A. |last3=Zhivotov |first3=A . I. |last4=Dibrivny |first4=A . V. |title=СОЗДАНИЕ СЕМЕЙСТВА КИСЛОРОДНО-КЕРОСИНОВЫХ ЖИДКОСТНЫХ РАКЕТНЫХ ДВИГАТЕЛЕЙ НА БАЗЕ ОТРАБОТАННЫХ ТЕХНОЛОГИЙ ДЛЯ ПЕРСПЕКТИВНЫХ РАКЕТ-НОСИТЕЛЕЙ ГП "КБ "ЮЖНОЕ" |journal=АВИАЦИОННО - КОСМИЧЕСКАЯ ТЕХНИКА И ТЕХНОЛОГИЯ |date=2013 |volume=2013 nr. 01 |issue=98 |pages=44–50 |url=http://www.khai.edu/csp/nauchportal/Arhiv/AKTT/2013/AKTT113/Degtyar.pdf |accessdate=2016-07-11 |trans-title=THE DEVELOPMENT OF LOX - KEROSENE L IQUID ROCKET ENGINES FAMILY FOR PERSPECTIVE LAUNCH VEHICLES OF YUZHNOYE SDO BASED ON PROVEN TECHNOLOGIES |publisher=National Aerospace university them. NE Zhukovsky |language=Russian |issn=1727-7337 |archive-url=https://web.archive.org/web/20160816211603/http://www.khai.edu/csp/nauchportal/Arhiv/AKTT/2013/AKTT113/Degtyar.pdf# |archive-date=2016-08-16 |url-status=dead }}</ref>
<ref name=khai-aktt201301p4450>{{cite journal |last1=Degtyarev |first1=A . V. |last2=Shulga |first2=V . A. |last3=Zhivotov |first3=A . I. |last4=Dibrivny |first4=A . V. |title=СОЗДАНИЕ СЕМЕЙСТВА КИСЛОРОДНО-КЕРОСИНОВЫХ ЖИДКОСТНЫХ РАКЕТНЫХ ДВИГАТЕЛЕЙ НА БАЗЕ ОТРАБОТАННЫХ ТЕХНОЛОГИЙ ДЛЯ ПЕРСПЕКТИВНЫХ РАКЕТ-НОСИТЕЛЕЙ ГП "КБ "ЮЖНОЕ" |journal=АВИАЦИОННО - КОСМИЧЕСКАЯ ТЕХНИКА И ТЕХНОЛОГИЯ |date=2013 |volume=2013 nr. 01 |issue=98 |pages=44–50 |url=http://www.khai.edu/csp/nauchportal/Arhiv/AKTT/2013/AKTT113/Degtyar.pdf |access-date=2016-07-11 |trans-title=THE DEVELOPMENT OF LOX - KEROSENE L IQUID ROCKET ENGINES FAMILY FOR PERSPECTIVE LAUNCH VEHICLES OF YUZHNOYE SDO BASED ON PROVEN TECHNOLOGIES |publisher=National Aerospace university them. NE Zhukovsky |language=ru |issn=1727-7337 |archive-url=https://web.archive.org/web/20160816211603/http://www.khai.edu/csp/nauchportal/Arhiv/AKTT/2013/AKTT113/Degtyar.pdf# |archive-date=2016-08-16 |url-status=dead }}</ref>
<ref name=ukrspexport-rd810>{{cite web |url=http://catalog.use.kiev.ua/index.php?action=setLang&lang=eng&search_val=&page=catalog&view=product&id=288&cat_id=&eid= |title=RD-810 |publisher=Defense Industry Of Ukraine Products And Services |accessdate=2016-07-11}}</ref>
<ref name=ukrspexport-rd810>{{cite web |url=http://catalog.use.kiev.ua/index.php?action=setLang&lang=eng&search_val=&page=catalog&view=product&id=288&cat_id=&eid= |title=RD-810 |publisher=Defense Industry Of Ukraine Products And Services |access-date=2016-07-11 |archive-date=2016-08-10 |archive-url=https://web.archive.org/web/20160810052802/http://catalog.use.kiev.ua/index.php?action=setLang&lang=eng&search_val=&page=catalog&view=product&id=288&cat_id=&eid= |url-status=dead }}</ref>
<ref name=yuzhnoye-rd810>{{cite web |url=http://www.yuzhnoye.com/en/technique/rocket-engines/marching/rd-810/ |title=RD-810 |publisher=Yuzhnoye |accessdate=2016-07-11 |archive-url=https://web.archive.org/web/20160709080323/http://www.yuzhnoye.com/en/technique/rocket-engines/marching/rd-810/# |archive-date=2016-07-09 |url-status=dead }}</ref>
<ref name=yuzhnoye-rd810>{{cite web |url=http://www.yuzhnoye.com/en/technique/rocket-engines/marching/rd-810/ |title=RD-810 |publisher=Yuzhnoye |access-date=2016-07-11 |archive-url=https://web.archive.org/web/20160709080323/http://www.yuzhnoye.com/en/technique/rocket-engines/marching/rd-810/# |archive-date=2016-07-09 |url-status=dead }}</ref>
}}
}}


==External links==
==External links==
* [http://www.yuzhnoye.com.ua Yuzhnoye Design Bureau English-language home page]
* [http://www.yuzhnoye.com.ua Yuzhnoye Design Bureau English-language home page] {{Webarchive|url=https://web.archive.org/web/20191123104231/https://yuzhnoye.com.ua/ |date=2019-11-23 }}


{{Rocket engines}}
{{Rocket engines}}

Latest revision as of 06:08, 7 May 2024

RD-810 (РД-810)
Country of originUkraine
DesignerYuzhnoye Design Bureau
ManufacturerYuzhmash
ApplicationFirst Stage
StatusIn development
Liquid-fuel engine
PropellantLOX / RP-1
Mixture ratio2.65
CycleStaged Combustion
Configuration
Chamber1
Performance
Thrust, vacuum2,105 kN (473,000 lbf)
Thrust, sea-level1,876 kN (422,000 lbf)
Chamber pressure18 MPa (2,600 psi)
Specific impulse, vacuum335.5 s (3.290 km/s)
Specific impulse, sea-level299 s (2.93 km/s)
Gimbal range8
Dimensions
Dry mass2,800 kg (6,200 lb)
References
References[1][2][3][4]

The RD-810 (РД-810) is a Ukrainian liquid propellant rocket engine burning LOX and Kerosene (RG-1) in a staged combustion cycle.[4] It has a single combustion chamber that provides thrust vector control by gimbaling of the nozzle in two axis by +/- 8°. It is being designed in Ukraine by Yuzhnoye Design Bureau for the prospective first stage propulsion of the Mayak rocket family.[4][2]

The RD-810 as well as the RD-801 are being designed based on the work of the RD-8 vernier and the maintenance and improvement of the RD-120 engines. The RD-810 can be used stand alone on a Mayak or could be used in a module of four called RD-810M to replace the RD-170 on the Zenit.[2]

See also

[edit]
  • Mayak – Prospective Ukrainian launch vehicle family for which the RD-810 is being developed.
  • RD-801 – A smaller engine of the same family designed by Yuzhnoe.
  • SCE-200 – An Indian rocket engine of equal specifications which might be based on the RD-810 blueprints.
  • Yuzhnoe Design Bureau – The RD-810 designer bureau.
  • Yuzhmash – A multi-product machine-building company that's closely related to Yuzhnoe and would manufacture the RD-RD-810.

References

[edit]
  1. ^ Brügge, Norbert (2016-07-11). "Ukrainian space-rocket and missile liquid-propellant engines". B14643.de. Retrieved 2015-08-06.[permanent dead link]
  2. ^ a b c Degtyarev, A . V.; Shulga, V . A.; Zhivotov, A . I.; Dibrivny, A . V. (2013). "СОЗДАНИЕ СЕМЕЙСТВА КИСЛОРОДНО-КЕРОСИНОВЫХ ЖИДКОСТНЫХ РАКЕТНЫХ ДВИГАТЕЛЕЙ НА БАЗЕ ОТРАБОТАННЫХ ТЕХНОЛОГИЙ ДЛЯ ПЕРСПЕКТИВНЫХ РАКЕТ-НОСИТЕЛЕЙ ГП "КБ "ЮЖНОЕ"" [THE DEVELOPMENT OF LOX - KEROSENE L IQUID ROCKET ENGINES FAMILY FOR PERSPECTIVE LAUNCH VEHICLES OF YUZHNOYE SDO BASED ON PROVEN TECHNOLOGIES] (PDF). АВИАЦИОННО - КОСМИЧЕСКАЯ ТЕХНИКА И ТЕХНОЛОГИЯ (in Russian). 2013 nr. 01 (98). National Aerospace university them. NE Zhukovsky: 44–50. ISSN 1727-7337. Archived from the original (PDF) on 2016-08-16. Retrieved 2016-07-11.
  3. ^ "RD-810". Defense Industry Of Ukraine Products And Services. Archived from the original on 2016-08-10. Retrieved 2016-07-11.
  4. ^ a b c "RD-810". Yuzhnoye. Archived from the original on 2016-07-09. Retrieved 2016-07-11.
[edit]
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