Accession Number:

AD0620073

Title:

FAST OPERATING VALVE FOR FEEDING A LIQUID, E.G., A FUEL COMPONENT INTO A LIQUID-PROPELLANT ROCKET ENGINE,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Report Date:

1965-06-29

Pagination or Media Count:

6.0

Abstract:

The object of the invention is a rapid-action valve for the feeding of a liquid, for example, the fuel component into a liquid-propellant rocket engine, which contains a body, a membrane covering the passage section of the flow part, and a membrane-piercing organ with a pyroactuator. For the purpose of lessening the weight while preserving the dependability the piroprovod fire duct is designed not connected in the power system with the body and separated from the flow part by a flexible diaphragm controlling the piercing organ and insulating the body from the highpressure gases. Author

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE