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Ion Propulsion Test Tube, R.H. Goddard

Air and Space Museum

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International media Interoperability Framework
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Object Details

Manufacturer

Dr. Robert H. Goddard

Summary

American rocket pioneer Robert Goddard (1882-1945) used this device between 1924 and 1928 in his experiments to determine the feasibility of ion propulsion for space travel. Ion engines, in which electrically charged particles of atoms are discharged, produce extremely high exhaust velocities. Because of that and potential long duration of operation, ion engines are ideal for deep space propulsion. However, they produce very low thrust and must be placed in space by conventional rocket boosters. Experiments in space with ion propulsion first took place in 1964.
Russell B. Hastings, one of Goddard's graduate students connected to his ion work, has identified this object in 1964 as "very likely a concentric screen device for detecting both plus and minus ion emissions." Mrs. Goddard gave it to the Smithsonian in 1965. It was later broken and partly lost as the Hastings states it was originally "two tubes with sealer and electrodes."

Credit Line

Gift of Mrs. Robert Goddard

Inventory Number

A19650296000

Restrictions & Rights

Usage conditions apply

Type

INSTRUMENTS-Scientific

Materials

Plastic
Glass
Rubebr
Coating
Wax
Paper
Copper Alloy

Dimensions

3-D (Tube): 15.2 × 2.5 × 2.5cm (6 × 1 × 1 in.)
Other (Wires): 48.3cm (1 ft. 7 in.)
3-D (Overall): 45.7 × 43.2 × 2.9cm, 1.5kg (1 ft. 6 in. × 1 ft. 5 in. × 1 1/8 in., 3.4lb.)

Country of Origin

United States of America

See more items in

National Air and Space Museum Collection

Data Source

National Air and Space Museum

Metadata Usage

Not determined

Link to Original Record

http://n2t.net/ark:/65665/nv9c28f3e14-476e-4a93-b513-8c9faf7c6034

Record ID

nasm_A19650296000

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