Maximum Takeoff Thrust
30.62 kN
Overall Pressure Ratio
21.95
Fuel Flow Take Off
0.347 kg/s
NOx Unitaryto CAEP8
77.3 % of limit
Architecture
| Fan |
Fan Stages
—
|
Fan Blades
—
|
Fan Technology
—
|
Fan Pressure Ratio
—
|
| Gearbox |
Geared Fan
No |
Gear
—
|
Reduction Ratio
—
|
| LP compressor |
Low-Pressure Compressor Stages
—
|
Low-Pressure Compressor Technology
—
|
BP Compressor Pressure Ratio
—
|
| IP compressor |
Intermediary-Pressure Compressor Stages
—
|
Intermediary-Pressure Compressor Technology
—
|
IP Compressor Pressure Ratio
—
|
| HP compressor |
High-Pressure Compressor Stages
—
|
High-Pressure Compressor Technology
—
|
HP Compressor Pressure Ratio
—
|
| Combustor |
Combustion Chamber
SABER-1 |
| HP turbine |
High Pressure Compressor Stages
—
|
High-Pressure Turbine Technology
—
|
| IP turbine |
Intermediary-Pressure Turbine Stages
—
|
Intermediary-Pressure Turbine Technology
—
|
| LP turbine |
Low-Pressure Turbine Stages
—
|
Low-Pressure Turbine Technology
—
|
| Whole engine |
Streams
2 |
Bypass Ratio
4.2 |
Overall Pressure Ratio
21.95 |
Afterburner
No |
Pictures
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All data (63 fields)
- Name
- HTF 7000 (AS907-1-1A)
- EASA ID
- 11HN002
- Aircraft Engine Manufacturer
- Honeywell
- Aircraft Engine Type
- Turbofan
- Fuel
- Jet A
- Geared Fan
- No
- Combustion Chamber
- SABER-1
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 4.2
- Overall Pressure Ratio
- 21.95
- Maximum Takeoff Thrust (kN)
- 30.62
- Hydrocarbon Take Off (g/kg fuel)
- 0.04
- Hydrocarbon Climb Out (g/kg fuel)
- 0.06
- Hydrocarbon Approach (g/kg fuel)
- 0.12
- Hydrocarbon Idle (g/kg fuel)
- 1.35
- Hydrocarbon Unitary Average (g/kN)
- 3.5
- Hydrocarbon Unitary Sigma (g/kN)
- 0.11
- Hydrocarbon Unitary Range (g/kN)
- 3.4-3.62
- Hydrocarbon Unitary Characteristic (g/kN)
- 5.4
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 27.5
- Carbon Monoxide Take Off (g/kg fuel)
- 0.6
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.6
- Carbon Monoxide Approach (g/kg fuel)
- 5.97
- Carbon Monoxide Idle (g/kg fuel)
- 34.5
- Carbon Monoxide Unitary Average (g/kN)
- 90.31
- Carbon Monoxide Unitary SD (g/kN)
- 1.6
- Carbon Monoxide Unitary Range (g/kN)
- 88.87-92.46
- Carbon Monoxide Unitary Characteristic (g/kN)
- 110.85
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 93.9
- NOx Take Off (g/kg fuel)
- 18.095
- NOx Climb Out (g/kg fuel)
- 16.28
- NOx Approach (g/kg fuel)
- 9.17
- NOx Idle (g/kg fuel)
- 3.98
- NOx Unitary Average (g/kN)
- 46.09
- NOx Unitary SD (g/kN)
- 0.79
- NOx Unitary Range (g/kN)
- 45.45-47.11
- NOx Unitary Characteristic (g/kN)
- 53.43
- NOx Unitaryto Standard (% of limit)
- 63.7
- NOx Unitaryto CAEP2 (% of limit)
- 79.6
- NOx Unitaryto CAEP4 (% of limit)
- 80.6
- NOx Unitaryto CAEP6 (% of limit)
- 81.1
- NOx Unitaryto CAEP8 (% of limit)
- 77.3
- Smoke Take Off (SN)
- 9.9
- Smoke Climb Out (SN)
- 9
- Smoke Approach (SN)
- 0.7
- Smoke Idle (SN)
- 1.7
- Smoke Max (SN)
- 9.92
- Smoke Sigma (SN)
- 0.42
- Smoke Range (SN)
- 9.2-10
- Smoke Characteristic (SN)
- 12.77
- Smoke Characteristicto Regulatory (% of limit)
- 39
- Fuel Flow Take Off (kg/s)
- 0.347
- Fuel Flow Climbout (kg/s)
- 0.288
- Fuel Flow Approach (kg/s)
- 0.104
- Fuel Flow Idle (kg/s)
- 0.048
- Fuel LTO (kg)
- 152
- Fuel Venting Compliant
- Yes
- Emissions Data Status
- C
- Emissions Data Superseded
- Yes
- Emissions Superseded By
- 11HN003
- Engine Status
- Out of production
- NOx Compliance Demonstration
- 2.3.2 d)