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Rocket Engine, Walter HWK 109-507

Air and Space Museum

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International media Interoperability Framework
IIIF provides researchers rich metadata and media viewing options for comparison of works across cultural heritage collections. Visit the IIIF page to learn more.
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Object Details

Manufacturer

Helmuth Walter KG

Summary

The firm of Helmuth Walter KG developed this hydrogen-peroxide rocket motor for the Henschel Hs 293 air-to-surface missile in 1940-42, based on several years of experience with assisted-take-off devices and rocket-aircraft engines. Hydrogen peroxide in 80% concentration (codenamed "T-Stoff") was mixed with a calcium permanganate catalyst ("Z-Stoff"), producing superheated steam and oxygen. The initial thrust of 600 kg (1300 lb.) declined to 400 kg (900 lb.) during the 10 second duration of the engine due to dropping air pressure from bottles that moved the propellants to the mixing chamber. This burst of thrust propelled the Hs 293 missile away from the launch aircraft and accelerated its glide to the target.
This engine came to the National Air and Space Museum in December 1975 along with a number of other rocket artifacts developed or tested after World War II by Reaction Motors, Inc.

Credit Line

Gift of Reaction Motors Div., Thiokol Chemical Corp.

Inventory Number

A19771225000

Restrictions & Rights

Usage conditions apply

Type

PROPULSION-Rocket Engines

Materials

Ferrous Alloys (Including Steel)
Aluminum Alloy
Paints
Glass
Plastics
Copper Alloys

Dimensions

3-D: 213.4 × 30.5 × 48.3cm (7 ft. × 1 ft. × 1 ft. 7 in.)
Storage (Including Wooden Crate): 117.5kg (259lb.)

Country of Origin

Germany

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/nv915fc8808-e0bc-4c15-8338-9f93681098a0

Record ID

nasm_A19771225000

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Rockets and Missiles

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Rockets and Missiles

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