Is a
Product attributes
Launch Date
2011
Founder
Industry
Product Parent Company
Single-chamber liquid rocket engine running on non-toxic components (kerosene + liquid oxygen).
Liquid rocket engine with afterburning of oxidizing gas
Fuel: Oxygen + kerosene
Modifications of the RD-191 engine
Development period 1999-2011
Purpose of the Angara PH
Number and period of launches 2 launches in 2014
The main stages of the RD-191 program
Conclusion of a contract with GKNPC im. Khrunicheva – 31.12.1998.
The development of design documentation was completed in 1999.
A mock-up was made for the Angara launch vehicle - March 1999.
The first fire test of RD-191 – July 27, 2001
RD-191 certification was completed in May 2011.
Timeline
No Timeline data yet.
