Lazy Sunday afternoon here. Decided to share some material I had ferreted away on the Pfalz D.III series performance in order to stir up some discussion. I've always considered the Pfalz to have been an unfairly criticized fighter.
Pfalz D.III / D.IIIa flight performance:
Peter L Gray's "The Pfalz D.III" (Profile Publications no.43), 1965:
British figures from a captured D.III (160 hp Mercedes)
Max. speed at 10,000 ft. 102.5 mph, at 15,000 ft. 91.5 mph. Climb to 5000 ft in 6 min., to 15,000 ft in 41 min. 20 sec.
German figures (not sourced)
Max. speed 165 km. hr. (103.12 mph). Climb to 1,000 m. (3,280 ft.) in 3.25 min., to 2,000 m (6,560 ft) in 7.25 min., to 3,000 m (9,840 ft.) in 11.75 min.
D.IIIa (175/180 hp Mercedes): at a loaded weight of 911 kg. (2,004 lb) made test climb to 5,000 m (16,400 ft.) in 33 min. on 4th Feb. 1918.
Author comments that:
"In service the Pfalz seems to have been a considerably maligned machine; many stories, probably most of them apocryphal, circulating as to its unsuitability: "too slow", "does not climb", "too heavy", "won't recover from a spin", "fuselage weak", "not properly constructed", "tail weak and liable to break off", etc. In actual fact it was quite a good, rugged aeroplane. Initially there was a tendency to failure of the upper wing wing-tips in combat…but stronger spars were ordered to rectify this. The Pfalz could dive a good deal faster than any other German fighter and with excellent stability, in consequence it provided a good gun platform. Its style of construction endowed it with an ability to absorb a fair degree of punishment. There certainly was a tendency for the machine to get in a flat spin from which it was exceedingly difficult to recover. In a report dated 25th October 1917, Jasta 24 expressed the following opinion…'It is slower than the Albatros D III; it is fast in a dive and is then faster than the Albatros D V. The climbing performance…varies greatly, sometimes almost as good as the average Albatros D V but never better'
Also: "The tailplane and one-piece unbalanced elevator were an angular, trapezoidal shape…The section was of inverse camber which gave stability in a prolonged dive and considerably assisted recovery"
- – - – -
Performance figures from Die deutschen Militärflugzeug 1910-1918, by Kroschel und Stutzer.
D.III D.IIIa.
climb:
1000m 3'17" -----
1500m 7'0"
3000m 11'45" -----
5000m ----- 33'0"
The Pfalz D.III & D.IIIa climb is better than the Alb.D.Va and slightly slower to 5000m than the Alb.D.V which gross weight was 915 kg. The Pfalz D.III weight was 932kg. The Pfalz D.IIIa was 934 kg. The Alb.D.Va was 957kg and the OAW built Alb.D.Va was 950kg.
The maximum airspeed was 165km/hr @ 3000m for the Pfalz D.III and D.IIIa which was exactly the same for the Alb.D.V, D.Va and alb.D.Va(OAW).
The ceiling was 5500 m for the Pfalz D.III and 6000 for the D.IIIa which is lower than the Alb.D.V @6500m and both Alb.D.Va machines @ 6250m.
B