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Energia-5K

Energia-5K


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Sodruzhestvo


Russia's future Moon rocket

During 2014, the concept of a Moon rocket proposed at RKK Energia around a year earlier continued to evolve. By that time, the project had received the designation Energia-5KV, where "V" stood either for "Vostochny launch site" or "vodorod," a Russian term for hydrogen. In the latter case, the name would emphasize more reliance on hydrogen fuel in the latest incarnation of the vehicle.

Previous chapter: Energia-5K rocket

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Energia-5KV

Above: RKK Energia's concept of the Energia-5KV rocket as of 2014.

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In the 2014 configuration, the lower stages of the Energia-5K rocket remained largely unchanged -- four boosters of the first stage with RD-170MV engines and a core booster of the second stage with an RD-171MV engine. All five boosters still shared a diameter of 4.1 meters. (The boosters were now distributed evenly around the core, instead of being attached in pairs as in the 2013 version of the rocket.)

However the rest of the vehicle saw a major revamp. The third stage was enlarged and switched from kerosene to the more potent hydrogen fuel. It would now be powered with four 40-ton-thurst RD-0150 engines, instead of a single one, producing a total thrust of 160 tons.

This upgrade alone increased the vehicle's payload to be delivered into a low Earth orbit from 75 tons in the original concept of the vehicle to 93 tons. Further improvements apparently promised to bump the payload to 95 tons.

The latest configuration of the orbital section of the rocket entering an initial parking orbit now included a two-stage space tug attached to a manned PTK NP spacecraft. The lower (fourth) stage dubbed Impuls-V relied on hydrogen fuel, even though its architecture was clearly inherited from RKK Energia's veteran Block-D upper stages. It would be equipped with a single 40-ton engine.

The Impuls-V stage would have the job of accelerating the PTK NP spacecraft from the low Earth orbit in the direction of the Moon or toward other destinations in deep space.

Following the Earth orbit escape maneuver, the Impuls-V stage would separate. It would leave the PTK NP spacecraft with a smaller fifth stage still attached. Known as Impuls-T, where "T" stands for "tormozhenie," Russian for "braking," the fifth stage would be used for a braking maneuver near a destination, for example, for inserting the PTK spacecraft into its lunar orbit. Unlike the two lower stages, Impuls-T would use storable hypergolic propellant and the S5.92 engine borrowed from the Fregat upper stage. (Possibly, there were also earlier proposals to use a modified Block-DM-03 stage with the 11D58MF engine in place of the Impuls-T stage.)

Known specifications of the Energia-5KV architecture:

-
Energia-5K (circa 2013)
Energia-5KV (circa 2014)
Liftoff mass
2,416 tons
2,425-2,470 tons
Payload mass to the low Earth orbit
approximately 79 tons
93.6-95.2 tons
Payload mass to the low Earth orbit, if Stage I boosters dropped 810 kilometeers downrange
-
100 tons
Payload mass to the low Earth orbit, if Stage I boosters dropped 1,370 kilometeers downrange
-
95.2 tons
Maximum payload mass delivered to 200-kilometer lunar polar orbit
-
24.0 tons
STAGE I (four strap-on boosters)
-
-
Propulsion system
Four boosters with four-chamber RD-170M engine each
Four boosters with four-chamber RD-170MV engine each
Stage diameter
4.1 meters
4.1 meters
Propellant mass
?
4x398 tons
Oxidizer
Liquid oxygen
Liquid oxygen
Fuel
Kerosene
Kerosene
Estimated burn time
161 seconds
161 seconds
STAGE II (Core stage))
-
-
Propulsion system
One RD-171M engine
One RD-171MV engine
Stage diameter
4.1 meters
4.1 meters
Propellant mass
?
398 tons
Oxidizer
Liquid oxygen
Liquid oxygen
Fuel
Kerosene
Kerosene
STAGE III
-
-
Propulsion system
One RD-191V engine
Four (4) RD-0150 engines
Stage diameter
4.1 meters
7.0 meters
Propellant mass
?
150 tons
Oxidizer
Liquid oxygen
Liquid oxygen
Fuel
Kerosene
Liquid hydrogen
Estimated burn time
240 seconds
?
STAGE IV
-
Impuls-V
Oxidizer
Liquid oxygen
Liquid oxygen
Fuel
Liquid hydrogen
Liquid hydrogen
Propellant mass
-
49.3 tons
Propulsion system
Two (modified) RD-0146D engines
One 40-ton engine
STAGE V
-
Impuls-T
Propellant mass
-
9.6 tons
Oxidizer
N/A
AT
Fuel
N/A
UDMH
Propulsion system
N/A
S5.92 (?)

Next chapter: Energia-5V/5VR

 

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RD-170

RD-170 engine. Click to enlarge Copyright © 2005 Anatoly Zak


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