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TsSKB Progress' super-heavy launchers


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Sodruzhestvo


Angara-100

Enisei

Above: A concept of the Yenisei-5 launch vehicle proposed by GKNPTs Khrunichev as early as 2008. Copyright © 2013 Anatoly Zak


Previous chapter: Angara-100 rocket

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Russian engineers draft super rocket

From the day the Soviet shuttle program was shut down in 1992, both Western and especially Russian press has been running occasional stories about a possible revival of the majestic Energia rocket or even the winged Buran orbiter. It was mostly a reflection of wishful thinking of the project's veterans, yet in 2012, the Russian space agency endorsed a long-term plan potentially leading toward a super-heavy launcher. Not surprisingly, by the time the big rocket appeared on the horizon, Russian engineers had already had their sketches ready.

Along with several other industry proposals, GKNPTs Khrunichev in Moscow, the manufacturer of the Proton rocket, drafted a pair of giant launchers designated Amur-5 and Yenisei-5. While Amur-5 was mostly a repackaged version of the Angara-100 design proposed back in 2005, Yenisei-5 featured a radically different approach. The concept was formulated as early as 2008.

Standing 75 meters tall, Yenisei-5 would use a core stage powered by three hydrogen-fed RD-0120 engines, which GKNPTs Khrunichev argued could be revived after the demise of the Energia rocket in the 1990s. Four RD-0120 engines propelled Energia's core stage.

The use of liquid hydrogen on the core stage as oppose to kerosene fuel would sharply increase the capability of the proposed launch vehicle, enabling it to deliver 125 tons to the low Earth orbit. The payloads to be sent beyond the initial low Earth orbit would be further increased by the use of hydrogen on a proposed space tug dubbed KVTK. It would serve as the third stage of the Yenisei-5 rocket.

The Yenisei-5 launch vehicle would be based at the yet-to-be-built launch site in Vostochny in the Russian Far East and become a centerpiece of an ambitious space program, possibly supporting a base on the Moon and even expeditions to Mars.

The central core stage on Yenisei-5 would ignite on the launch pad simultaneously with four kerosene-fueled strap-on boosters equipped with existing RD-170 engines. GKNPTs Khrunichev also promised that the diameter of the first stage modules would allow their transportation by rail. This claim was in contradiction with a quoted diameter of the first stage -- 4.1 meters. Although GKNPTs Khrunichev routinely transports Proton stages of that diameter to Baikonur launch site, such trip to the Russian Far East would probably be impossible without major re-building of railway lines, tunnels and other infrastructure, as well as stopping and diverting head-on traffic -- hardly a realistic option. It was a key reason why the diameter of the cancelled Rus-M rocket was restricted to 3.8 meters.

GKNPTs Khrunichev was not the first company to propose reviving the technology and architecture of the Energia rocket, which could deliver around 100 tons to the low Earth orbit. During the 2007-2008, RKK Energia also studied a configuration closely resembling the legendary vehicle, which differed from its Soviet predecessor by the placement of the payload section at the top of the rocket, rather than in a side-mounted container. However, at the time, the company's planners ultimately decided to limit their even most ambitious plans by payloads not exceeding 60 tons.

Yet in 2012, the Russian space agency, Roskosmos, appeared to endorse GKNPTs Khrunichev's proposals, at least in its long-term paper plans. In December, Gennady Raikunov, the head of TsNIIMash research institute responsible for long-term strategy of the Russian space program, told the Interfax-AVN news agency, that the first launch of the super-heavy rocket based on Amur and Yenisei designs would take place from Vostochny in 2028.

The implementation of such a program would require huge investments. According to many Russian rocket propulsion experts, the RD-0120 engine would have to be developed essentially from scratch, as most of its critical infrastructure was no longer existing. The rocket would also need a monumental new launch facility. Serious logistical challenges to transporting large-diameter core stage or its components from the factory to the launch site would have to be addressed. Since traditional Russian method of transporting rockets by rail would not be an option, a large transport aircraft and associated facilities would have to be developed. Still, proponents of hydrogen propulsion argued that Russia, like any other space-faring nation, would have no alternative to the ultimate rocket fuel.

Alternative architectures

By 2013, RKK Energia in Korolev and TsSKB Progress in Samara, the manufacturer of the Soyuz and Energia rockets, were both revising their own concepts of super-heavy vehicles. While RKK Energia's designs were known to be based on the Sodruzhestvo concept, revived a year earlier, TsSKB Progress was yet to unveil its architecture. In March, the head of the company, Aleksandr Kirilin told a local news network that TsSKB Progress would propose Roskosmos a heavy launcher with a payload of 70 tons within a month. He added that any ambitious exploration program aiming the Moon or Mars would need two launchers with payloads of 70 and 130 tons. According to Kirilin, TsSKB Progress, along with RKK Energia and GKNPTs Khrunichev had been studying such designs. (639)

The propulsion alternatives

Although most designs of heavy and super heavy rockets in Russia relied on tried and tested RD-170, RD-180 and RD-0124 engines, new engine designs were also under consideration. In April 2012, the Interfax AVN news agency reported that RKK Energia and Keldysh Center proposed Scientific and Technical Council at Roskosmos to consider the use of the RD-175 engine, then under development at NPO Energomash in Moscow, whithin the project of a super-heavy rocket. Few details on RD-175 were available, besides its whooping 1,000 tons of thrust. A designation indicated that it might be derived from RD-170/171 and, thus, used liquid oxygen and kerosene. At the time, NPO Energomash completed the preliminary design of the engine and was assembling an experimental unit to test its key design features. (640)

Next chapter: Sodruzhestvo rocket

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APPENDIX

 

Known capabilities of the Yenisei-5 launch vehicle (as of 2012):

Payload to a 200-kilometer orbit with an inclination 51.8 degrees toward the Equator
125 tons
Relative mass of the payload to the mass of the launch vehicle
5.21 percent
Payload mass to geostationary orbit
30 tons
Payload toward the Moon with a single launch
49 tons
Payload toward the Moon during a two-launch flight scenario
65 tons
Launch mass
2,397 tons
Mass of payload fairing
7 tons
Stage I
-
Stage I propellant load
1,520 tons
Stage I propulsion system
Four (4) RD-170 engines
Stage I thrust (on the Earth surface)
2,960 tons
Stage II
-
Stage II propellant load
548 tons
Stage II propulsion system
Three (3) RD-0120 engines
Stage II thrust (in vacuum)
570 tons

 

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Story, illustrations and photography by Anatoly Zak

Last update: July 30, 2013

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Yensei-5

Yenisei-5 rocket. Copyright © 2013 Anatoly Zak


Tail

The core stage of the Energia rocket and its tail section accommodating propulsion system (bottom). Copyright © 2000 Anatoly Zak


Energia

View of the tail section of the Energia's core stage with four main engines. Copyright © 2001 by Anatoly Zak


engine

The main engines of the Energia's core stage. Four engines were powering the Energia rocket. A single engine would be sued in Energia-M version of the vehicle. Copyright © 2001 Anatoly Zak


RD-170

The RD-170 engine powered the first stage of the Energia rocket. Click to enlarge: 300 by 400 pixels / 56K Copyright © 2005 Anatoly Zak

 

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