OpenAP engine properties
OpenAP / Junzi Sun · Retrieved 2026-09-05
LGPL-3.0; source dataset includedROLLS-ROYCE
Trent 895
Turbofan
ENGINE9 documented fields
OpenAP reference record 5RR040. 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 thrust413050 N
Bypass ratio5.7 :1
Pressure ratio41.52 :1
Takeoff fuel flow4.03 kg/s
REFERENCE COVERAGELoading coverage…
PROVENANCE1 linked source
LAST RETRIEVED2026-09-05
View missing fields and source dates
Source editions
OpenAP engine properties ↗Edition / 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 · 5RR040 · max_thrust
- 413,050 N
02
Architecture
- Bypass ratioOpenAP engine dataset · 5RR040 · bpr
- 5.7 :1
- Overall pressure ratioOpenAP engine dataset · 5RR040 · pr
- 41.52 :1
03
Fuel flow
- Approach fuel flowOpenAP engine dataset · 5RR040 · ff_app
- 1.05 kg/s
- Climb-out fuel flowOpenAP engine dataset · 5RR040 · ff_co
- 3.19 kg/s
- Idle fuel flowOpenAP engine dataset · 5RR040 · ff_idl
- 0.33 kg/s
- Reference LTO fuelOpenAP engine dataset · 5RR040 · fuel_lto
- 1,357 kg
- Takeoff fuel flowOpenAP engine dataset · 5RR040 · ff_to
- 4.03 kg/s
04
Provenance
- Source manufacturer nameHistorical source label retained.
- Rolls-Royce plc
Aircraft connections
Exact engine-name matches in the aircraft catalogue. This is not a complete installation or certification list.
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.