The “Pause-Mücke”, designed by Adalbert Schmid, a two-seater sports and touring aircraft developed in 1939, did not get beyond a prototype due to the war.
Engine: Salmson AD 9
Span: 10.00 m
Length: 6,40 m
Flying weight: 480 kg
Max. speed: 145 km/h
This monoplane was built by Firma Max Pause in Heidelberg, Germany, probably in 1909 and probably powered by an Antoinette engine.
Single seat single engined high wing monoplane with two axis control (optional conventional three axis control). Wing has unswept leading edge, swept forward trailing edge and tapering chord; cruciform tail. Pitch control by elevator on tail; yaw control by fin mounted rudder; no separate roll control (optional roll control by ailerons); control inputs through stick for pitch/yaw and (optionally) pedals for roll. Wing braced from below by struts; wing profile; double surface. Undercarriage has three wheels in tail dragger formation; bungee suspension on all wheels. Push right go right tailwheel steering connected to yaw control. No brakes. Aluminium tube/steel tube framework, without pod. Engine mounted below wing driving pusher propeller. Framework in 2024T3 aluminium and 4130 chrome moly steel. Wing covering is Stits Polyfiber, doped.
Shown for the first time to the public at 0shkosh in August 1982, P Craft from D Paup appears to be a minimum aircraft and as such is directly descended from the Kolb Flyer and Ron Wheeler Scout.
This one offers the choice between two axis control, with steering by induced roll, or conventional three axis control when fitted with ailerons (an option on the standard kit). Where the lower longeron and a higher, nearly parallel tube which carries the pilot seat meet at the nose, there is a horizontal transverse tube on which can be hinged the rudder pedals.
Paup aircraft offers the two axis version in kit form, requiring 150 hours for completion, at the price of $3395 in 1983.
Engine: Cuyuna 215D, 20hp at 6000rpm
Propeller diameter and pitch 36 x 12 inch, 0.91 x 0.30 m
No reduction
Power per unit area 0.15hp/sq.ft, 1.6hp/sq.m
Fuel capacity 2.5 US gal, 2.1 Imp gal, 9.5 litre
Wing span 32.5 ft, 9.88 m
Total wing area 132 sq.ft, 12.3 sq.m
Wing aspect ratio 8.0/1
Main wheels diameter overall 20 inch, 51 cm
Empty weight 165 lb, 75kg
Max take off weight 402 lb, 182 kg
Payload 237 lb, 107 kg
Max wing loading 3.05 lb/sq.ft, 14.8 kg/sq.m
Max power loading 20.1 lb/hp, 9.1 kg/hp
Max level speed 60 mph, 97 kph
Never exceed speed 70 mph, 113 kph
Max cruising speed 50 mph, 80 kph
Economic cruising speed 35 mph, 56 kph
Stalling speed 22 mph, 35 kph
Max climb rate at sea level 300ft/min, 1.5m/s
Take off distance 75 ft, 23 m
Albert Paulson, of Northwood ND., USA, built the single-place Aeronef, or Gold Bug, in 1910.
Built on the box-kite principle, with the forward box used for changing the angle of flight, while the rear box was adjusted for the direction of flight. Made its public appearance at the June 1910 Indianapolis Air Meet, but not known if it flew.
The Companhia Aeronáutica Paulista CAP-9 Carioca four-seat, single-engine high-wing monoplane with enclosed cockpit and fixed undercarriage, was CAP’s last attempt, in 1947, to remain in the aircraft market. The company had chosen to build the CAP-9 Carioca instead of the CAP-8. The CAP-8 (which reached the prototype stage) was a 4-seater low-wing aircraft and although the prototype was made of wood in order to gain time (the war was about to end but there was still a shortage of aluminum), the idea was to build an all-metal aircraft.
Without commercial success with its new projects and a vertiginous drop in its orders, CAP ends its activities in 1948.
The Companhia Aeronáutica Paulista CAP-8 of 1944 was a four-seat, single-engine low-wing monoplane with enclosed cockpit and fixed (retractable planned in series aircraft) undercarriage, inspired by Messerschmitt Bf 108 Taifun. Only one was built.
A high-wing cabin monoplane
An improved version was later built by Nieva.
The four-seat Paulic XT3-B NX21726 was originally built in 1939 as a joint project of John W. Thorp and Rudy Paulic. A side-by-side trainer planned for Boeing School of Aeronautics in Oakland, where both Paulic and Thorp worked.
It was dismantled after several test flights and stored until July 1958, when it was redesigned and rebuilt by Paulic as four-place retractable-gear T-3B-1 with a 190hp Lycoming O-435 engine and re-registered NX6497C.
XT3-B NX21726
Engine: 125hp Warner Scarab
Wingspan: 33’0″
Length: 23’6″
Useful load: 1060 lb
Max speed: 144 mph
Cruise: 122 mph
Stall: 58 mph
seats: 2
T-3B-1 NX6497C
Engine: 190 hp Lycoming O-435-A
Span: 32 ft 11 in
Length: 22 ft
Wing area: 132 sq.ft
AUW: 2500 lb
Useful load: 1100 lb
Max speed: 170 mph
Cruise: 155 mph
ROC: 1200 fpm
Range: 800 mi
Seats: 4
As Paulat did not succeed in obtaining the required second Hilz engine for his seaplane, he designed the light 1912 Hydro-Aero Monoplane – suited for one Hilz engine – and completed in June 1912 as a landplane. This machine crashed on June 6, 1912.
Paulat was called under arms during the Balkan War (1912-1913), but once returning, decided to end his aeronautical work due to his financial difficulties.
Ion Paulat built the first Romanian seaplane in 1911. As the Ministry of War provide no assistance to him, Paulat had difficulties obtaining an engine to power the aeroplane. In the end – through friendly help in order to conduct a flight test – he obtained one of the two 55 hp Hilz engines needed. With one engine the machine flew in early November 1911, making a jump of 10 meters at a height of 35 centimetres.
As Paulat did not succeed in obtaining the required second Hilz engine, he designed the light 1912 Hydro-Aero Monoplane – suited for one Hilz engine
