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Flow Indicator, Liquid Oxygen, Rocket Engine, R.H. Goddard

Display Status:
This object is not on display at the National Air and Space Museum, it is either on loan or in storage.

Flow Indicator, Liquid Oxygen, Rocket Engine, R.H. Goddard

 

  • Summary

Manufacturer:   Dr. Robert H. Goddard

Country of Origin: United States of America

Dimensions:
3-D Test: 41.9 x 6.7 x 30.5cm (16 1/2 x 2 5/8 x 12 in.)

Materials:
Steel, Brass, Felt, Copper, Natural Fabric, Cardboard, Plastic

This is a flow regulator for liquid oxygen, also called a lox [flow] indicator, and was used by Robert H. Goddard for some of his earliest liquid fuel rocket experiments, about 1923-1924.

Mrs. Robert H. Goddard donated this object to the Smithsonian Institution in 1959 as part of a large collection of artifacts from her husband.

Gift of Mrs. Robert H. Goddard


Inventory number: A19590080000