RD-810

From Wikipedia, the free encyclopedia
Jump to navigation Jump to search
RD-810 (РД-810)
Country of originUkraine
DesignerYuzhnoye Design Bureau
ManufacturerYuzhmash
ApplicationFirst Stage
StatusIn development
Liquid-fuel engine
PropellantLOX / RG-1
Mixture ratio2.65
CycleStaged Combustion
Configuration
Chamber1
Performance
Thrust (vac.)2,105 kN (473,000 lbf)
Thrust (SL)1,876 kN (422,000 lbf)
Chamber pressure18 MPa (2,600 psi)
Isp (vac.)335.5 s (3.290 km/s)
Isp (SL)299 s (2.93 km/s)
Gimbal range8
Dimensions
Dry weight2,800 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). National Aerospace university them. NE Zhukovsky. 2013 nr. 01 (98): 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. Retrieved 2016-07-11.
  4. ^ a b c "RD-810". Yuzhnoye. Archived from the original on 2016-07-09. Retrieved 2016-07-11.

External links[edit]