General Electric GE4
![](../I/m/General_Electric_GE4_1.JPG)
A mock-up of the GE4/J5 single-shaft afterburning turbojet
![](../I/m/Ge4_sst.jpg)
GE4
The General Electric GE4 turbojet engine was designed in the late 1960s as the powerplant for the Boeing 2707 supersonic transport. The GE4 was a nine-stage, single-shaft, axial-flow turbojet based largely on the General Electric YJ93 which powered the North American XB-70 bomber.[1] The GE4 was the most powerful engine of its era, producing 50,000 lbf (220 kN) dry, and 65,000 lbf (290 kN) with afterburner.[2] The Boeing 2707 was cancelled in 1971, putting an end to further work on the GE4.
Specifications (GE4/J5P)
Data from [3][4]
General characteristics
- Type: Turbojet
- Length: 27ft 4 in (833.1cm)
- Diameter: 5ft 11 in (180.3cm)
- Dry weight: 11,300 lb (5,100 kg)[5]
Components
Performance
Other Specifications
- Compressor inlet diameter: 60.6 in (1,539 mm)[5]
- Exhaust nozzle diameter: 74.2 in (1,880 mm)
- Core airflow: 620 lb (280 kg) per second
- Noise:
- Takeoff: 104 dB
- Sideline: 117 dB
- Approach: 107 dB
See also
- Related development
- Comparable engines
- Related lists
References
|
---|
| General | |
---|
| Military | |
---|
| Accidents / incidents | |
---|
| Records | |
---|
| Misc. | |
---|
|