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re: Pictures of old Russian rocket, I have no idea what the article says
Posted on 4/16/17 at 5:55 pm to DavidTheGnome
Posted on 4/16/17 at 5:55 pm to DavidTheGnome
It looks like a prototype to the buran launch vehicle
Posted on 4/16/17 at 5:59 pm to willymeaux
It's called Energia.
Energia (Russian: ???????, Energiya, "Energy") was a Soviet rocket that was designed by NPO Energia to serve as a heavy-lift expendable launch system as well as a booster for the Buran spacecraft. Control system main developer enterprise was the NPO "Electropribor".[2][3] The Energia used four strap-on boosters each powered by a four-chamber RD-170 engine burning kerosene/LOX, and a central core stage with 4 one-chamber RD-0120 (11D122) engines fueled by liquid hydrogen/LOX.[4]
The launch system had two functionally different operational variants: Energia-Polyus, the initial test configuration, in which the Polyus system was used as a final stage to put the payload into orbit, and Energia-Buran,[5] in which the Buran spacecraft was the payload and the source of the orbit insertion impulse.
The rocket had the capacity to place about 100 tonnes in Low Earth orbit, up to 20 tonnes to geostationary orbit and up to 32 tonnes to a translunar trajectory.[1]
Energia (Russian: ???????, Energiya, "Energy") was a Soviet rocket that was designed by NPO Energia to serve as a heavy-lift expendable launch system as well as a booster for the Buran spacecraft. Control system main developer enterprise was the NPO "Electropribor".[2][3] The Energia used four strap-on boosters each powered by a four-chamber RD-170 engine burning kerosene/LOX, and a central core stage with 4 one-chamber RD-0120 (11D122) engines fueled by liquid hydrogen/LOX.[4]
The launch system had two functionally different operational variants: Energia-Polyus, the initial test configuration, in which the Polyus system was used as a final stage to put the payload into orbit, and Energia-Buran,[5] in which the Buran spacecraft was the payload and the source of the orbit insertion impulse.
The rocket had the capacity to place about 100 tonnes in Low Earth orbit, up to 20 tonnes to geostationary orbit and up to 32 tonnes to a translunar trajectory.[1]
This post was edited on 4/16/17 at 6:00 pm
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