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RD-0120

RD-0120 is a science topic covered in the lgStudy science library. This page brings together a partial reference excerpt, illustrations, worked examples, real-world applications and a short study plan, so you can understand RD-0120 rather than just read about it. In short: The RD-0120 (Russian: Ракетный Двигатель-0120, romanized: Raketnyy Dvigatel-0120, lit. 'Rocket Engine 0120', GRAU index: 11D122) was the Energia core rocket engine, fueled by LH2/LOX, roughly equivalent to the RS-25 (Space Shuttle Main Engine, SSME). These were attached to the Energia core rather than the orbiter, so were not recoverable after a flight, but created a more modular design (the Energia core could be us…

RD-0120 — main illustration
RD-0120 — illustration

Key takeaways

  • RD-0120 belongs to science; place it in that map before memorising details.
  • Learn the definition first, then one example that makes the definition concrete.
  • Connect RD-0120 to a quantity you can measure, compute or draw — that is where exam questions come from.
  • Reproduce the core statement of RD-0120 from memory before moving on to harder problems.

Reference excerpt

The RD-0120 (Russian: Ракетный Двигатель-0120, romanized: Raketnyy Dvigatel-0120, lit. 'Rocket Engine 0120', GRAU index: 11D122) was the Energia core rocket engine, fueled by LH2/LOX, roughly equivalent to the RS-25 (Space Shuttle Main Engine, SSME). These were attached to the Energia core rather than the orbiter, so were not recoverable after a flight, but created a more modular design (the Energia core could be used for a variety of missions besides launching the shuttle). The RD-0120 and the RS-25 have both similarities and differences. The RD-0120 achieved a slightly higher specific impulse and combustion chamber pressure with reduced complexity and cost (but it was single-use), as compared to the RS-25. It uses a fuel-rich staged combustion cycle and a single shaft to drive both the fuel and oxidizer turbopumps. Some of the Russian design features, such as the simpler and cheaper channel wall nozzles, were evaluated by Rocketdyne for possible upgrades to the RS-25. It achieved combustion stability without the acoustic resonance chambers that the RS-25 required.

Specifications

RD-0120 Thrust at 106% throttle (vacuum): 1,961.3 kN (200 tf; 441,000 lbf), (sea-level): 1,526 kN (155.6 tf; 343,100 lbf) Specific impulse (vacuum): 455 seconds (4.46 km/s), (sea-level): 354 seconds (3.47 km/s) Burn time: nominal 480–500 s, certified for 1670 s Basic engine weight: 3,450 kg (7,610 lb) Length: 4.55 m, diameter: 2.42 m Propellants: LOX / LH2 Mixture ratio: 6:1 Contractor: Chemical Automatics Design Bureau (Конструкторское Бюро Химавтоматики) Vehicle application: Energia core stage.

See also RD-170 — the rocket engine used on Energia's strap-on boosters

References

External links Molniya Research & Industrial Corporation's Buran page (english) RD-0120 details (in Russian) Energiya Booster details (in Russian)

Illustrations

RD-0120 illustration

Worked examples

Example 1 — a first encounter with RD-0120

Start with the simplest possible case. Write down what RD-0120 claims or describes in one sentence, then invent the smallest concrete situation in which that sentence is true. In science, the smallest case is usually a single object, a single equation or a single measurement. Check that every symbol or term in your sentence has a meaning in that case.

Example 2 — changing one variable

Take the situation from Example 1 and change exactly one quantity: double it, halve it, or set it to zero. Predict what should happen to RD-0120 before you calculate. Comparing your prediction with the result is the fastest way to find out whether you understand the idea or only the words.

Example 3 — an exam-style question

Typical questions about RD-0120 ask you to (a) state it precisely, (b) apply it to given data, and (c) explain a limitation. Practise writing all three answers in under five minutes; the third part is what separates a full-mark answer from an average one.

Applications of RD-0120

In research
RD-0120 appears in science research whenever the underlying quantities have to be modelled precisely. Papers usually cite it as a starting assumption and then explore where it breaks down.
In technology and industry
Engineering practice reuses RD-0120 in design rules, simulations and safety margins. Knowing the idea lets you read a specification sheet and understand why the numbers look the way they do.
In the classroom
RD-0120 is common in secondary-school and first-year university syllabi. It links to neighbouring topics 1980s rocket engines, KBKhA rocket engines, Rocket engines of the Soviet Union, so understanding it makes those chapters shorter.
In everyday life
Look for RD-0120 outside the textbook — in sport, cooking, traffic, electronics or the sky above you. An example you found yourself is remembered far longer than one you were given.
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How to study RD-0120 in 20 minutes

  1. Read the reference excerpt below once, without taking notes.
  2. Close the page and write down what RD-0120 means in your own words.
  3. Compare your version with the excerpt and mark what you missed.
  4. Work through the three examples above with pen and paper.
  5. Explain RD-0120 out loud to somebody else — or to Teacher Smith in the lgStudy chat.

Frequently asked questions

What is RD-0120 in simple terms?

The RD-0120 (Russian: Ракетный Двигатель-0120, romanized: Raketnyy Dvigatel-0120, lit. 'Rocket Engine 0120', GRAU index: 11D122) was the Energia core rocket engine, fueled by LH2/LOX, roughly equivalent to the RS-25 (Space Shuttle Main Engine, SSME). These were attached to the Energia core rather t…

Why does RD-0120 matter?

Because it connects several science ideas at once: it gives you a definition you can apply, a quantity you can calculate, and a way to check whether a result is plausible.

How should I study RD-0120?

Read the excerpt, restate it from memory, then work through the examples and applications listed on this page. The five-step study plan above takes about twenty minutes.

What does this page cover?

It gives you a compact reference excerpt plus original lgStudy explanations, examples, applications and study material on RD-0120.

Tags

  • 1980s rocket engines
  • KBKhA rocket engines
  • Rocket engines of the Soviet Union
  • Rocket engines using hydrogen propellant
  • Rocket engines using the staged combustion cycle
  • Soviet inventions

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