Engine vznikol other vývojom engineand RM2, got the chamber prídavného spaľovania and označenie RM2A.
The first years with motorom RM2A graduated prototype SAAB J 29D of the day 20.3.1954.
Other modifications of the engineand a final verzia engineand with the designation of the RM2B that poháňala lietadlá SAAB J 29F. Licenčná production version of RM2 and RM2B prebiehala in rokoch 1952-1955.
Technical information:
Výrobca: Svenska Flygmotor AB (SFA), according to the bible
Type (Type): jednoprúdový (Turbojet)
Dĺžka (Lenght) : 3073 mm (121 in)
Priemer (Diameter): 1346 mm (53 in)
Dry hmotnosť (Dry weight): 1139 kg (2.530 lb)
Part of the engineand (Components):
Compressor (Compressor): single stage odstredivý (Single stage centrifugal flow)
Spaľovacia chamber (Combustors): 10 komôr (10 chambers)
Turbine (Turbine): Single-stage (Single-stage)
Fuel (Fuel type) : kerosene (Kerosene)
Performance (Performance):
Maximálny ťah (Maximum thrust): 27,4 kN pri 10250 rpm (of 6,200 lb at 10.250 rpm) with prídavným spaľovaním, of 21.12 kN (4750 lb at 10.250 rpm) without prídavného spaľovania
Source:
www.airpowerworld.info
Mike Spick - The Illustrated Directory of Fighters - books.google.sk/books?isbn=0760313431
www.flightglobal.com.
The first years with motorom RM2A graduated prototype SAAB J 29D of the day 20.3.1954.
Other modifications of the engineand a final verzia engineand with the designation of the RM2B that poháňala lietadlá SAAB J 29F. Licenčná production version of RM2 and RM2B prebiehala in rokoch 1952-1955.
Technical information:
Výrobca: Svenska Flygmotor AB (SFA), according to the bible
Type (Type): jednoprúdový (Turbojet)
Dĺžka (Lenght) : 3073 mm (121 in)
Priemer (Diameter): 1346 mm (53 in)
Dry hmotnosť (Dry weight): 1139 kg (2.530 lb)
Part of the engineand (Components):
Compressor (Compressor): single stage odstredivý (Single stage centrifugal flow)
Spaľovacia chamber (Combustors): 10 komôr (10 chambers)
Turbine (Turbine): Single-stage (Single-stage)
Fuel (Fuel type) : kerosene (Kerosene)
Performance (Performance):
Maximálny ťah (Maximum thrust): 27,4 kN pri 10250 rpm (of 6,200 lb at 10.250 rpm) with prídavným spaľovaním, of 21.12 kN (4750 lb at 10.250 rpm) without prídavného spaľovania
Source:
www.airpowerworld.info
Mike Spick - The Illustrated Directory of Fighters - books.google.sk/books?isbn=0760313431
www.flightglobal.com.