RD-843

RD-843 (РД-843)
Country of origin Ukraine
First flight 2012-02-13
Designer Yuzhnoye Design Bureau
Manufacturer Yuzhmash
Application Upper Stage
Associated L/V Vega
Predecessor RD-869
Status In Production
Liquid-fuel engine
Propellant N2O4 / UDMH
Mixture ratio 2.0
Cycle Pressure Fed
Configuration
Chamber 1
Performance
Thrust (vac.) 2.452 kilonewtons (551 lbf)
Chamber pressure 20.4 MPa (2,960 psi)
Isp (vac.) 315.5 seconds
Burn time up to 667s
Dimensions
Dry weight 15.93 kilograms (35.1 lb)
Used in
AVUM
References
References [1][2][3]

The RD-843 is a Ukrainian single nozzle liquid propellant rocket engine burning pressure-fed UDMH and nitrogen tetroxide. It is rated for up to 5 restarts, and can gimbal up to 10 degrees in each direction.[2]

It was developed by Yuzhnoye Design Bureau for Avio and is manufactured by Yuzhmash. It uses the RD-869 thrust chamber, the old Soviet ICBM SS-18 Satan final stage engine from which it is evolved, and which was also designed by Yuzhnoye. The RD-843 ground test campaign included 74 tests, 140 ignitions, reaching a total of 8201 s, which is approximately 12 service lives on 4 engines. As of May 2015 it has been successfully used on four orbital launches.[2]

It is currently used as the main engine of Vega's AVUM upper stage. Germany’s aerospace technology agency-DLR is understood to be keen to work with the Italians to develop a replacement for the RD-843.[4][5]

See also

References

  1. "Liquid rocket engine RD-843". Yuzhmash. Retrieved 2015-05-29.
  2. 1 2 3 "RD-843". Yuzhnoye. Retrieved 2015-05-29.
  3. "RD-843". Defense Industry Of Ukraine Products And Services. Retrieved 2016-07-11.
  4. Clark, S. (2012-02-14). "Vega launcher program courts German participation". Spaceflight Now. p. 1. Retrieved 2015-05-29.
  5. Thisdell, Dan (2014-04-24). "ESA keeps eye on Ukraine crisis as Vega launch nears.". Flightglobal. Retrieved 2015-05-29.
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