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Float Light

7 pp

3-D (Diameter x Length): 7.3 × 21cm (2 7/8 × 8 1/4 in.)

#ld1-1643400021979-1643400022744-1

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Flow Regulator, Liquid Oxygen, Rocket Engine, R.H. Goddard, 1926

7 pp

This liquid oxygen flow regulator was tested by the American rocket pioneer Robert H. Goddard (1882-1945) about July 1926. There were two of these devices, each placed on the ends of liquid oxygen pipes. Within each regulator (within the cylindrical cage formed by the regulators) Goddard placed a cork. As the liquid oxygen flowed through these pipes, a certain amount of condensation was allowed to

#ld1-1643400021979-1643400022918-0

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Focke-Achgelis Fa 330A-1 Bachstelze (Water Wagtail)

6 pp

The Fa-330 was stowed in two tubes of approximately 3.75 meters (12 ft 4in) length built vertically into the U-boat's conning tower. One tube contained the blades and tail and the other contained the fuselage. Four crewmen could assemble the entire structure in three minutes in calm conditions. Rotation of the blades in preparation for flight could be done by hand, but if a course pitch (which pro

#ld1-1643400021979-1643400022434-0

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Fokker D.VII

4 pp

Upon winning the Adlershof competition, Fokker received a production order for 400 Fokker D.VIIs. Concerned that the Fokker factory would be unable to meet the demand for the new fighter, IdFlieg (Inspektion der fliegertruppen), directed Albatros, (Fokker's great rival) to produce D.VIIs under license. Albatros built the Fokker D.VII at both its Johannisthal and Schneidemühl factories, known as Al

#ld1-1643400021979-1643400022021-0

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Fokker T-2

5 pp

The third and successful attempt was made from east to west. Kelly and Macready took off from the combined Roose-velt-Hazelhurst Field on Long Island, New York, at 12:30 p.m., eastern standard time. At takeoff, the airplane had a gross weight of 4,932 kg (10,850 lb)-only 68 kg (150 lb) less than the T-2's specified limit of 4,990 kg (11,000 lb). Lieutenant Kelly was at the controls first, and flew

#ld1-1643400021979-1643400022027-0

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Fokker T-2 Instrument Panel

1 pp

Height 49.5 cm (19.5 in.), Width 29.2 cm (11.5 in.), Depth 10.2 cm (4 in.)

#ld1-1643400021979-1643400039677-0

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Force Measuring Unit, Skylab

6 pp

3-D: 45.7 × 42.5 × 16.4cm (1 ft. 6 in. × 1 ft. 4 3/4 in. × 6 7/16 in.)

#ld1-1643400021979-1643400033075-0

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Force Measuring Unit, Skylab

6 pp

3-D: 45.7 × 41.9 × 22.9cm (1 ft. 6 in. × 1 ft. 4 1/2 in. × 9 in.)

#ld1-1643400021979-1643400033073-1

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Ford 5-AT Tri-Motor

21 pp

3-D: 1518.9 × 591.8 × 416.6cm, 4352.7kg (49 ft. 10 in. × 19 ft. 5 in. × 13 ft. 8 in., 9596lb.)

#ld1-1643400021979-1643400026988-0

object

Forward Hoist Fitting

1 pp

Other (Overal ): 4 1/2 in. × 8 in. × 1 ft. 5 in. (4 1/2 in. × 8 in. × 1 ft. 5 in.)

#ld1-1727944212747-1727944236145-2

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Fowler-Gage Biplane

10 pp

At least four Gage biplanes were constructed. They were flown by four well-known aviators of the day, Roy Francis, Phil 0. Parmalee, J. Clifford Turpin, and Robert G. Fowler, all of whom were trained at the Wright school or flew on the Wright exhibition team. Each airplane was initially fitted with a 60-horsepower Hall-Scott engine and a 2.1 m (7 ft) propeller. The upper wing had a span of 13 m (4

#ld1-1643400021979-1643400022372-0

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Frankfort TG-1A (Cinema)

7 pp

Stan Corcoran's TG-1A (Training Glider Model 1A) was the first aircraft selected to train U.S. Army glider pilot cadets to fly the Waco CG-4A combat assualt glider. The Waco could be difficult to handle with heavy loads, and a skilled pilot was required to fly it. Until late in the war, Wacos were only produced in limited numbers, and none were available for training. Before bidding on producing t

#ld1-1643400021979-1643400034198-0

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Float Light

Flow Regulator, Liquid Oxygen, Rocket Engine, R.H. Goddard, 1926

Focke-Achgelis Fa 330A-1 Bachstelze (Water Wagtail)

Fokker D.VII

Fokker T-2

Fokker T-2 Instrument Panel

Force Measuring Unit, Skylab

Force Measuring Unit, Skylab

Ford 5-AT Tri-Motor

Forward Hoist Fitting

Fowler-Gage Biplane

Frankfort TG-1A (Cinema)