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Engine, Ramjet, Marquardt C20-0.85

Air and Space Museum

Object Details

Manufacturer

Marquardt Aircraft Company, Los Angeles, California

Physical Description

Type: Ramjet
Thrust: 6,672 N (1,500 lb) at 0.85 Mach Number
Configuration: 3 fuel injection points just inside entrance to diffuser; crossed-lattices type flame holder
Weight: 56.7 kg (125 lb)

Summary

Marquardt Corporation was one of the few aeronautical engineering firms dedicated almost solely to the development of the ramjet. Its designs were developed through the 1940s into the 1960s, but the ramjet concept never became a major product, and Marquardt turned to other fields in the 1970s. It suffered a particularly bad financial crisis with the ending of the Cold War, and went bankrupt in the 1990s.
The C20-.85 was an athodyd-type ramjet, produced in 1946, using ram air for compression. It was designed for subsonic flight using thrust obtainable from combustion of fuel, and intended as an aircraft auxiliary power plant and expendable missile engine.
The C20-.85 powered the Martin Gorgon IV testbed, developed in 1946 as an air-to-surface missile, and later used as a target drone. The Gorgon IV was considered the U.S.'s first successful ramjet missile, although it never became operational.

Credit Line

Transferred from the U.S. Navy

Date

Circa 1946

Inventory Number

A19710923000

Restrictions & Rights

Usage conditions apply

Type

PROPULSION-Turbines (Jet)

Materials

Aluminum
Steel
Copper Alloy
Magnesium Alloy
Paint
Anodized Aluminum
Cadmium Plating

Dimensions

Overall: 125lb., 50.8cm (56.7kg, 1 ft. 8 in.)
Storage: 241.3 × 76.2 × 76.2cm (7 ft. 11 in. × 2 ft. 6 in. × 2 ft. 6 in

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/nv991b33c65-0cd6-416a-8726-04fe97c8d523

Record ID

nasm_A19710923000

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