The 1928 Thomson M-1 single-place open cockpit, high wing monoplane was planned to be marketed as a lightplane for $2,000. It got no further. Only one built.
Engine: Anzani
Wingspan: 20’0″
Length: 10’3″
Max speed: 121 mph
Cruise: 105 mph
Stall: 32 mph
In 1931 Milford H Thompson produced the Midget single-place open cockpit shoulder-wing monoplane, registered N12067, and powered by a 29hp Harley Davidson engine.
Engine: Harley Davidson, 29 hp
Speed: 75 mph
Empty weight: 350 lb
Take-off run: 175 ft
In 1928 Milford H Thompson produced a single place open cockpit, parasol wing monoplane, powered by a 29hp Harley-Davidson engine. It was capable of 65 mph.
The 1914 Thompson-Day was designed by D L Thompson and C H Day as a two-place open cockpit biplane powered by a 90hp Gyro Duplex.
It set altitude record of 15,580′ in 1914. Thompson was also often photographed flying this plane in competition with race cars.
Built by Charles H Day at Griffith Park, Los Angeles CA., the 1915 Thompson Biplane was powered by an 80 hp rotary engine. Thompson had been looping the plane successfully.
The two place cabin monoplane A-2 Sport N717Y built by Walter J Thomas in 1931 was powered by a 55hp Michigan Aero engine.
The A-1 Sport built by Walter J Thomas c.1930 was a single place, open cockpit biplane. Two were built, N7112 powered by a 30hp Anzani, and N12921 with a 27hp Heath-Henderson engine.
The Thomas-Morse TM-24 of 1924 was an all-metal, corrugated-skin pursuit improvement over the TM-23, but still had enough design problems to result in rejection by the Army after McCook Field tests (as P-380).
With bridge-truss struts and biplane tail, the sole example built was dismantled and stored away.
Engine: 440hp Curtiss D-12
Wingspan: (upper) 25’0″ (lower) 30’1″
Length: 20’5″
Useful load: 1500 lb
Max speed: 143
Cruise speed: 114 mph
Stall: 63 mph
Wing chord: 63″ upper, 52″ lower
Seats: 2
The one Thomas-Morse M-23 built, in 1923, for Army evaluation was a single place open cockpit biplane. All-metal, corrugated-skin pursuit design, it had inherent design and cooling problems despite several modifications. It was evaluated at McCook Field but rejected for its flight characteristics and high landing speed. It was dismantled in 1926.
Engine: Curtiss D-12, 440 hp
Wingspan: 19’6″ (later 23’0″)
Length: 16’8″ (later 17’6″)
Useful load: 788 lb
Max speed: 167 mph
Cruise speed 125 mph
Stall: 80 mph
Range: 280 mi
Ceiling: 20,150′
Seats: 1
The 1915 Thomas-Morse SH-4 was a USN float version of the Thomas T-2 with a single main pontoon and wingtip floats, larger tail, three-bay wings, and various engines including the Curtiss OX-5 and Hisso A.
The first design for Thomas-Morse by B D Thomas, it incorporated much of the same look as his Curtiss J, and sold for $7,575.
Fifteen were built; A134 to 136, and A395 to 406.
Wingspan: 44’0″
Length: 29’9″
Useful load: 897 lb
Speed: 83 mph
All Aero 