Argus As 014

Maximum Takeoff Thrust

3.53 kN

Diameter

546.1 mm

Length

3657.6 mm

Dry Weight

170 kg

Thrust To Weight

2.12

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 —
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 1	Bypass Ratio —	Overall Pressure Ratio —	Afterburner No

No pictures yet for this family.

Name	Aircraft Engine	Number of Engines	Length (m)	Flat Wing Span (m)
Messerschmitt Me 328	Argus As 014	2	7.17	6.9

Name	Aircraft Engine Manufacturer	Maximum Takeoff Thrust (kN)
BMW 109-558	BMW	3.7	Compare
TEM Toloue-4	TEM (Turbine Engine Manufacturing)	3.7	Compare
Turbomeca Arbizon	Turbomeca	3.73	Compare

All data (14 fields)

Name: Argus As 014
Aircraft Engine Manufacturer: Argus Motoren
Aircraft Engine Type: Pulsejet
Dry Weight (kg): 170
Diameter (mm): 546.1
Length (mm): 3657.6
Wikipedia Article (URL): en.wikipedia.org/wiki/Argus_As_014
Fuel: Gasoline
Geared Fan: No
Afterburner: No
Streams: 1
Maximum Takeoff Thrust (kN): 3.53
Thrust To Weight: 2.12
Compressor Description: None, compression was achieved acoustically, with additional ram pressure when in flight.