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ROLLS-ROYCE

BR700-710A2-20

Mixed-flow turbofan

ENGINE9 documented fields
Compare this engine
OpenAP reference record 4BR009. Values describe the source configuration and test conditions. Fuel-flow modes are reference test points, not an in-flight fuel prediction. Dimensions and certified operating limits are not supplied by this dataset.
Reference thrust65610 N
Bypass ratio4.19 :1
Pressure ratio24.16 :1
Takeoff fuel flow0.714 kg/s
REFERENCE COVERAGELoading coverage…
PROVENANCE1 linked source
LAST RETRIEVED2026-09-05
View missing fields and source dates

Source editions

OpenAP engine propertiesEdition / snapshot: Reference snapshot, September 2026Retrieved: 2026-09-05

Retrieval dates record when Owl obtained the data; they are not publication dates or proof that a specification is current. Where the edition contains only a snapshot date, the original publication date is not recorded.

01

Output

Reference maximum thrustOpenAP engine dataset · 4BR009 · max_thrust
65,610 N
02

Architecture

Bypass ratioOpenAP engine dataset · 4BR009 · bpr
4.19 :1
Overall pressure ratioOpenAP engine dataset · 4BR009 · pr
24.16 :1
03

Fuel flow

Approach fuel flowOpenAP engine dataset · 4BR009 · ff_app
0.214 kg/s
Climb-out fuel flowOpenAP engine dataset · 4BR009 · ff_co
0.595 kg/s
Idle fuel flowOpenAP engine dataset · 4BR009 · ff_idl
0.089 kg/s
Reference LTO fuelOpenAP engine dataset · 4BR009 · fuel_lto
299 kg
Takeoff fuel flowOpenAP engine dataset · 4BR009 · ff_to
0.714 kg/s
04

Provenance

Source manufacturer nameHistorical source label retained.
Rolls-Royce Deutschland

Aircraft connections

Exact engine-name matches in the aircraft catalogue. This is not a complete installation or certification list.

No exact aircraft connection documented in this dataset.

Dimensions, dry weight, shaft-power ratings and certified limits are not documented in this engine dataset.

Sources & context

Reference values vary with model, rating and conditions. Consult the relevant manufacturer documentation for certified specifications.