RB211
Embed This Widget
Add the script tag and a data attribute to embed this widget.
Embed via iframe for maximum compatibility.
<iframe src="https://planefyi.com/iframe/entity//" width="420" height="400" frameborder="0" style="border:0;border-radius:10px;max-width:100%" loading="lazy"></iframe>
Paste this URL in WordPress, Medium, or any oEmbed-compatible platform.
https://planefyi.com/entity//
Add a dynamic SVG badge to your README or docs.
[](https://planefyi.com/entity//)
Use the native HTML custom element.
Technical Specifications
- Thrust
- 270,0 kN (60 600 lbf)
- Bypass Ratio
- 4,3:1
- Fan Diameter
- 2,192 m
- Pressure Ratio
- 33,0:1
- SFC
- 0,3400 lb/lbf·h
- Dry Weight
- 4 479 kg
- Length
- 3,175 m
- First Run
- 1969
- In Service
- 1972
Overview
The Rolls-Royce RB211 is one of the most historically significant jet engines ever built. Developed in the 1960s as a competitor for the Lockheed L-1011 TriStar programme, the RB211 pioneered the three-spool engine architecture that would define the Rolls-Royce Trent family for decades. It also nearly destroyed the company: the enormous cost of developing its revolutionary composite fan blades, combined with a fixed-price contract, drove Rolls-Royce into insolvency in 1971 — leading to nationalisation by the British government.
Despite its turbulent birth, the RB211 proved to be an exceptional engine. Its three-spool layout, titanium and carbon-fibre materials (the composite fan blades were ultimately replaced with titanium), and advanced aerodynamics delivered performance that set new industry benchmarks. The RB211-535 variant became the sole engine for the Boeing 757, accumulating an outstanding reliability and safety record over more than 30 years of production.
Technical Specifications
| Specification | Value |
|---|---|
| Thrust (max) | 270 kN / 60,600 lbf |
| Bypass ratio | 4.3:1 |
| Fan diameter | 2.192 m (86.3 in) |
| Overall pressure ratio | 33:1 |
| Dry weight | 4,479 kg |
| Length | 3.175 m |
| SFC (cruise) | 0.3400 lb/(lbf·h) |
| First run | 1969 |
| In service | 1972 |
Variants
- RB211-22B: Original production variant for the L-1011 TriStar at 42,000 lbf, incorporating titanium fan blades after the composite design was abandoned.
- RB211-524: Significantly uprated variant at 53,000–60,600 lbf for the Boeing 747-200/-300/-400, featuring an enlarged fan and improved core.
- RB211-535C/E4: Extensively redesigned variant for the Boeing 757, with a new fan, a two-stage intermediate-pressure turbine, and improved fuel efficiency. The -535E4 was the definitive 757 engine, powering the aircraft for United Airlines, Delta, British Airways, and many others.
Aircraft Applications
- Lockheed L-1011 TriStar — launch application
- Boeing 747-400 (RB211-524 series)
- Boeing 757-200 (RB211-535 series)
- Boeing 757-300 (RB211-535 series)
Development History
Rolls-Royce launched the RB211 in 1966 after winning the Lockheed L-1011 engine contract. The programme was technically audacious: the three-spool layout was unprecedented in commercial aviation, and the use of Hyfil carbon-fibre composite fan blades was ahead of its time. When bird-strike testing shattered the composite blades, Rolls-Royce was forced to redesign them in titanium, absorbing enormous additional costs on a fixed-price contract. The company filed for bankruptcy in February 1971. The British government nationalised Rolls-Royce within weeks, judging the engine manufacturer too strategically important to allow to fail. The RB211 entered service with Eastern Air Lines on the L-1011 in 1972. The RB211-535, developed for the 757, became the direct ancestor of the Trent family: Rolls-Royce stretched and developed the RB211 core progressively from the 1970s through the 1990s, eventually producing the Trent 700, Trent 800, Trent 900, and Trent 1000.