Nikite Wraith

The Nikite/Gold Marque Sports Wraith 260/Shadow 176 was a single seat single engined flex wing aircraft with weight shift control, Rogallo wing with keel pocket. Pilot suspended below wing in trike unit, using bar to control pitch and yaw/roll by altering relative positions of trike unit and wing. Wing braced from above by kingpost and cables, from below by cables; floating cross tube construction with 66% double surface enclosing cross tube; pre¬formed ribs. Undercarriage has three wheels in tricycle formation; no suspension on any wheels. Push right go left nosewheel steering independent from yaw control. No brakes. Aluminium tube trike unit, with optional pod. Engine mounted below wing driving pusher propeller.

Designed by Dave Nick¬els, the Wraith 260 trike unit is a mono pole design and is intended for use with Gold Marque Sports’ Shadow 176 wing.

An all new combination, the trike unit first flew in April 1983.

The trike unit is distinctive in that instead of the normal folding seat frame, the seat frame slides complete, along a runner on the bottom tube. When rigged, the frame is held at the rearward end of the runner by a pin.
The company standardised on Hunting engines, the choice for the single seater being the single-¬cylinder HS260A, which has electric start as standard. The Wraith 260 trike unit came ready to-¬fly or as a kit. The kit has 90% of the holes drilled in the main frame and is ready for the engine to bolt on.

The Nikite/Southdown Sailwings Wraith 525/Lightning DS is the same as the Wraith 260/Shadow except: Tan¬dem two seater. Rogallo wing with fin. >75 % double surface.

Most companies start off building single seaters and then move on to dual machines, but with Nikite the reverse occurred, as the Wraith 525 trike unit was actually first flown before the 260. This mono pole two seater first took to the air in October 1982 and has been designed to be compatible with two Rogallos the Chargus Titan and the Southdown Sailwings Lightning DS. Unlike the single seater, the 525 was not designed in house but by John Sharpe, a North¬ampton enthusiast who handed the design over to Nikite for production. There are obvious similarities to the solo machine, particularly as regards make of engine and seat stowing mechanism. Like the solo, it was sold either ready to fly or as a kit.

Wraith 260/Shadow 176
Engine: Hunting HS260A, 25 hp at 6000 rpm
Prop¬eller diameter and pitch 52x27inch, 1.32×0.69m
V belt reduction, ratio 2.3/1
Max static thrust 175 lb, 79 kg
Power per unit area 0.14 hp/sq.ft, 1.5hp/sq.m
Fuel capacity 2.7 US gal, 2.3 Imp gal, 10.2 litre
Wing span 35.5ft, 10.82 m
Chord at root 8.2ft, 2.50 m
Chord at tip 3.0 ft, 0.91 m
Dihedral 0.7 degrees
Nose angle 130 degrees
Keel pocket depth 1.0 ft, 0.30 m
Total wing area 176 sq.ft, 164 sq.m
Keel pocket area 3.0 sq.ft, 0.28 sq.m
Wing aspect ratio 7.2/1
Wheel track 4.5 ft, 1.37 m
Wheelbase 5.2 ft, 1.57 m
Nosewheel diameter overall 12 inch, 30 cm
Main wheels diameter overall 12 inch, 30 cm
Empty weight 174 lb, 79kg
Max take off weight 388 lb, 176kg
Payload 214 lb, 97kg
Max wing loading 2.20 lb/sq.ft, 10.7kg/sq.m
Max power loading 15.5 lb/hp, 7.0kg/hp

Wraith 525/Lightning DS
Engine: Hunting HS525A, 45 hp at 6000 rpm
Propeller diameter and pitch 52 x 30 inch, 1.32×0.76m
V belt reduction, ratio 2.0/1
Max static thrust 250 lb, 113kg
Power per unit area 0.23 hp/sq.ft, 2.5 hp/sq.m
Fuel capacity 2.7 US gal, 2.3 Imp gal, 10.2 litre
Length overall 11.2 ft, 3.35 m
Wing span 34.5 ft, 10.52 m
Chord at root 8.0ft, 2.44m
Chord at tip 3.5ft, 1.07m
Anhedral 1.5 degrees
Nose angle 130 degrees
Fin height 3.3 ft, 1.01 m
Total wing area 195 sq.ft, 18.1 sq.m
Wing aspect ratio 6.3/1
Wheel track 5.2ft, 1.57 m
Wheelbase 6.0ft, 1.83 m
Nosewheel diameter overall 12 inch, 30 cm
Main wheels diameter overall 12 inch, 30 cm
Empty weight 231 lb, 105 kg
Max take off weight 641 lb, 291 kg
Payload 410 lb, 186 kg
Max wing loading 3.29 lb/sq.ft, 16.1 kg/sq.m
Max power loading 14.2 lb/hp, 6.5kg/hp
Load factors +4.0, 2.0 design; +6.0, 3.0 ulti¬mate

Nihon University N-58 Cygnet

The students of Nihon University, under the leadership of Dr Hidemasa Kimura, have designed and built two light aircraft. The second is a high-wing four-seat light-plane known as the N-58 Cygnet.

Although the Cygnet bears a close resemblance to the Piper Tri-Pacer, it is a new design utilizing existing Tri-Pacer components only in its undercarriage, engine mounting and control systems. Construction is all-metal, with fabric covering, and it is powered by a 140 hp Lycoming O-290-D2 engine.

Span: 35 ft 2 in
Length: 22 ft 11 in
Height: 8 ft 9 in
Wing area: 185 sq.ft
Gross weight: l,950 lb
Empty weight: l,256 lb
Max speed: 117 mph
Econ cruising speed: 93 mph at 6,600 ft
Stalling speed: 42 mph
Service ceiling: 14,800 ft
TO to 50ft: 1,250 ft
Landing from 50ft: 1,440 ft
Max range 10% res: 445 miles

Nihon University Okamura N-52

The students of Nihon University, under the leadership of Dr Hidemasa Kimura, have designed and built two light aircraft. The first was the Okamura N-52 low-wing monoplane, which flew on April 7, 1953.

Designed by Professor H. Kimura, the N-52 was powered by a 65 hp Continental C65. The N-52 is of mixed construction with fabric covering.

Engine: 65 hp Continental C65
Wingspan: 28 ft 2.5 in
Wing area: 129 sq.ft
Length: 19 ft 8 in
Height: 8 ft 6 in
Empty weight: 660 lb
Loaded weight: 1100 lb
Max speed: 108 mph at SL
Cruise: 101 mph
ROC: 550 fpm
Range: 305 mi

Nihon Z1G3

Under JASDF contract, Japan Aircraft Manufacturing Co carried out a lengthy high-lift research programme with a much-modified Saab-91B Safir.
With the designation Z1G3, this aircraft has a 260 h.p. Continental IO-470-D engine, reduced span of 31ft 6in, blown flaps, large trailing-edge fillets, slotted tailplane and other changes to give it STOL performance.