Rumpler C.IV / 6B 2 / Pfalz C.I

The Rumpler C.IV was a German single-engine, two-seat reconnaissance biplane. It was a development of C.III with different tail surfaces and using a Mercedes D.IVa engine in place of the C.III’s Benz Bz.IV. The Rumpler 6B 2 was a single-seat floatplane fighter variant with a 120 kW (160 hp) Mercedes D.III engine built for the Kaiserliche Marine (Imperial Navy).

For a two-seater reconnaissance aircraft, Rumpler C.IV had an excellent performance, which enabled it to remain in front-line service until the end of World War I on the Western Front, as well as in Italy and Palestine. Its exceptional ceiling allowed pilots to undertake reconnaissance secure in the knowledge that few allied aircraft could reach it.

300 aircraft were licence-built by Pfalz Flugzeugwerke as the Pfalz C.I, differing in ailerons on all four wings. From February 1917 they were renamed Rumpler C.IV (Pfal).

Replica
Slingsby T.58 Rumpler C.IV

Rumpler C.IV
Powerplant: 1 × Mercedes D.IVa, 190 kW (260 hp)
Propeller: 2-bladed fixed-pitch
Wingspan: 12.66 m (41 ft 6 in)
Wing area: 33.5 m2 (361 sq ft)
Length: 8.41 m (27 ft 7 in)
Height: 3.25 m (10 ft 8 in)
Empty weight: 1,080 kg (2,381 lb)
Gross weight: 1,530 kg (3,373 lb)
Maximum speed: 171 km/h (106 mph, 92 kn) at 500 m (1,640 ft)
Endurance: 3½-4 hr
Service ceiling: 6,400 m (21,000 ft)
Crew: 2 (pilot and observer)
Guns: 1 × fixed, 7.92 mm (.312 in) LMG 08/15 and 1 × 7.92 mm (.312 in) Parabellum MG14 machine gun
Bombs: 100 kg (220 lb)

Rozé, Perret et Chaffal 1910 biplane

The Roze, Perret, et Chaffal biplane was a large overhung biplane that might have been designed by Francois Denhaut and was made partly of steel tubing. It had a single trapezoidal tailplane aft only and no apparent vertical surfaces. The arrangement of the two pusher propellers was similar to that on the Wright. It was damaged in 1909 at Poitiers, and probably rebuilt into the photographed configuration, which was tested at Poitiers, France, in May 1910.

Royal Aircraft Factory AE.3 / RAM

The last aircraft type to emerge from the Royal Aircraft Factory at Farnborough, before its change of name in June 1918 to Royal Aircraft Establishment, the A.E.3 was itself an extrapolation from the N.E.1.

Designated as an “Armoured Experimental” type, the A.E.1 was intended as a specialised ground-attack fighter, for which purpose it was to mount a pair of 7.7mm Lewis guns in the nose, with a limited degree of movement in azimuth and depression. A third Lewis was to be pillar-mounted in the front, observer’s, cockpit for self-defence. Like the N.E.1, the A.E.3 was a large three-bay equi-span biplane, differing principally in the construction and shape of the nacelle, which was armoured with steel plate and provided stowage for 32 ammunition drums.

Royal Aircraft Factory AE.3 / RAM Article

Intended to be powered by the 200hp Hispano engine as used in the N.E.1, the A.E.3 prototype emerged at the end of March 1918 with a 200hp Sunbeam Arab, whilst the second, eight weeks later, had a 230hp Bentley B.R.2 rotary. Flight testing of the latter began on 4 June, and larger ailerons and rudders were fitted before this A.E.3 went to France for service trials, which aroused little enthusiasm. The third aircraft, also completed in June 1918, had an Arab engine like the first and in this form the A.E.3 was named the Ram I, whilst the B.R.2 version became the Ram II.

A proposed derivative, the Ram III, was not built and no production ensued, other, better, types having become available.

AE.3 / Ram Mk. 1
Engine: 1 x 200-h.p. Sunbeam Arab
Span: 47ft 10.5in
Length: 8.44 m / 28 ft 8 in
Height: 3.05 m / 10 ft 0 in
Wing area: 52.02 sq.m / 559.94 sq ft
Max. speed: 153 km/h / 95 mph
Seats: 2

Ram Mk. II
Engine: 1 x 230-h.p. Bentley B.R.2.
Span: 47ft 10.5in
Seats: 2

Royal Aircraft Factory A.E.3 Ram

Royal Aircraft Factory NE.1

As a derivative of the F.E.9, the RAF planned to develop a dedicated night fighter as the F.E.12. This was to have used the same 200hp Hispano- Suiza eight-cylinder Vee-type water-cooled engine, the same undercarriage, tailbooms, tail unit and wing centre section as the F.E.9, and basically the same nacelle, but with the crew positions reversed. New equi-span, three-bay wings were planned, with plain unbalanced ailerons. The pilot, in the front cockpit for the best possible view during unaided nocturnal operations, was to have a forward-firing 7.7mm Lewis gun, whereas the observer was to be armed with a Vickers rocket gun for which two mounts were to be provided for firing forwards or aft. Provision was to be made for a searchlight in the nose, and another on the forward mount for the rocket gun, with a winddriven generator under the nacelle. Six prototypes were planned, but before construction began the designation was changed to N.E.1 (for “Night-flying Experimental”) and some changes were made. These eliminated the second searchlight, increased the span of the wing centre section, changed the tail unit design, moved the boom attachment points on the tailplane outwards, and introduced a wide-track undercarriage with a divided axle arrangement.

Flown early in September 1917, the first N.E.1 was almost immediately damaged and was then modified, before resuming flying on 4 October, to accommodate the observer in the front cockpit with the rocket gun and the pilot behind with a fixed Lewis gun. In this form, the N.E.1 was submitted to official trials at Martlesham Heath in November 1917, but was not thought to have adequate performance to serve as a night fighter. The other five prototypes were all completed by January 1918, but one was used only for static testing, another probably remained unflown and only one was issued to an RFC squadron for home defence.

Engine: 1 x 200-h.p. Hispano-Suiza
Wingspan: 14.57 m / 47 ft 10 in
Length: 9.19 m / 30 ft 2 in
Height: 2.94 m / 10 ft 8 in
Wing area: 51.57 sq.m / 555.09 sq ft
Max take-off weight: 1336 kg / 2945 lb
Empty weight: 939 kg / 2070 lb
Max. speed: 153 km/h / 95 mph
Ceiling: 5335 m / 17500 ft
Seats: 2