Aerospace Engines A to Z
Aerospace Engines A to Z

Updated: 09-May-2018

EFW

(Switzerland)


EFW engine specifications

EFW was a Swiss engine factory that made engines under license and from own design. As they also built aircraft cells, this company was remarkably independent.

-For the EFW N-20 aircraft, it manufactured the "AS Mamba" renamed "Swiss Mamba" and with reference SM-01.

-The turbofan SM-05 gave 1,500 Kgs of thrust. We are waiting for more documentation.

From Appendix 6: During a visit to the Transport Museum in Luzern in 2008, the "Swiss-Mamba" was found, which was developed from the English AS Mamba, but instead of being a turboprop, a Fan was adapted.

-It was the first double-flow reactor that was made at the EFW workshops (also known as F + W).

-Situated in Emmen near Luzern, (Lucerne).

-Due to the Swiss characteristic of having three official languages, it was known as "Fabrique Fedérale d'Avions", as "Fabbrica Federale d'Aeroplani" and in the local language -Emmen-, in German "Eidgenössisches FlugzeugWerk".

EFW, Swiss-Mamba for the N-20
"Swiss-Mamba for the N-20"

-Destined to the Swiss N-20 "Aiguillón" aircraft, of the flying wing type.

EFW, One of the two fan outlets
"One of the two fan outlets"

-As we can see, the engine accessories are not upon or under the engine but on both sides, due to the aircraft design.

EFW, Side outlet and combustion chambers
"Side outlet and combustion chambers"

EFW, Exhaust nozzle with afterburner
"Exhaust nozzle with afterburner"

-It was calculated to deliver 1,700 Kgs of thrust with additional combustion in the exhaust (Afterburner).

-The development of this project was canceled in 1952. As well as those of the engines SM-03, SM-04 and SM-05, in favor of buying foreign material from the East and the West, considering the Czech Mig-15, the Saab J-29 or the French Mystere IV.

-Finally the main acquisition was 100 English Hunters in 1958.

-The SM-01 that was bound for the Swiss indigenous N-20 Aiguillón fighter plane built by EFW itself, had four of these engines. Taking advantage of the excess air of the compressor to create a post-combustion in the nozzle and the cold air of the fan for a high-lift and reverse as directed by different channels.

EFW, Swiss-Mamba SM-01 cross-section
"Swiss-Mamba SM-01"

-The SM-03 was an improved SM-01 but insufficient. It had a compressor designed by Brown-Boveri & Cie.

-The next version in this project was the SM-04 and like the previous one, the LP compressor had gear. The LP compressor provided both primary and secondary air at the same time.

-The SM-05 had the characteristic of having two shafts or contra-rotating turbines: the HP had one stage and the LP had two stages.

EFW, Swiss-Mamba SM-05 cross-section
"Swiss-Mamba SM-05"

-There was still an SM-06, similar to the SM-04, for which we have no details at the moment.

-We located another SM-01 at the Zurich Museum, interesting turbofan based on the English turboprop Mamba.

EFW, Swiss-Mamba SM-01
"Swiss-Mamba SM-01"

Engines of EFW

Model: SM-01, Swiss Mamba

Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:

Other details:
EFW, Swiss-Mamba SM-01

"EFW, Swiss-Mamba SM-01"

Model: SM-03, Swiss Mamba

Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:

Other details:
Model: SM-04, Swiss Mamba

Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:

Other details:
Model: SM-05, Swiss Mamba

Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:

Other details:
EFW, Swiss-Mamba SM-05 diagram

"EFW, Swiss-Mamba SM-05 diagram"