Hello
I dig a bit deeper into FAF D.XXI speed and climb.
A couple figures based on test flights, both took off weighting 1970 kg. Both datasets are took from graphs published in secondary sources, espesially that of FR-96 was a bit difficult, background being purely white and graphs being rather small.
First FR-107, which was one of maybe only 4 which got Mercury VIII during the war and test was flown when it was powered by Mercury VIII.
Climb to 5000 m 6'08", to 6000 m 7'53"
Max speed 352kmh at SL and 413kmh at 5000m.
FR-96, engine Mercury VII, max power 810-840 hp at 4420 m 2750rpm. Take off power at SL 728 hp at 2750rpm. On ground adjustable Ratier airscrew 3.0m diameter, reduction gear 0.666
Climb to 5000 m 7'12", to 6000 m 9'36"
Max speed 353kmh at SL and 416kmh at 4750m
Sources: Lentäjän näkökulma II
Ilmailu Joulukuu 1989
Suomen Ilmailuhistoriallinen Lehti 4/2000
First 2 for FR-96 and the latter for FR-107.
Juha
I dig a bit deeper into FAF D.XXI speed and climb.
A couple figures based on test flights, both took off weighting 1970 kg. Both datasets are took from graphs published in secondary sources, espesially that of FR-96 was a bit difficult, background being purely white and graphs being rather small.
First FR-107, which was one of maybe only 4 which got Mercury VIII during the war and test was flown when it was powered by Mercury VIII.
Climb to 5000 m 6'08", to 6000 m 7'53"
Max speed 352kmh at SL and 413kmh at 5000m.
FR-96, engine Mercury VII, max power 810-840 hp at 4420 m 2750rpm. Take off power at SL 728 hp at 2750rpm. On ground adjustable Ratier airscrew 3.0m diameter, reduction gear 0.666
Climb to 5000 m 7'12", to 6000 m 9'36"
Max speed 353kmh at SL and 416kmh at 4750m
Sources: Lentäjän näkökulma II
Ilmailu Joulukuu 1989
Suomen Ilmailuhistoriallinen Lehti 4/2000
First 2 for FR-96 and the latter for FR-107.
Juha