Accession Number:

AD0264516

Title:

Problem of the Strength of ZHRD (Liquid-Fuel Rocket Engine) Burner with Connected Envelopes

Descriptive Note:

[Technical Report, Annual Report]

Corporate Author:

AIR FORCE SYSTEMS COMMAND WRIGHT-PATTERSON AFB OH

Personal Author(s):

• DUBENETZ, S.A.

Report Date:

1961-08-28

Pagination or Media Count:

23

Abstract:

Investigations of certain problems associated with the strength and resistance of the cylindrical part of the ZhR burner with connected envelopes were carried out during 1954-1956 at the MAI Moscow Aviation Institute. They included both theoretical and experimental research. One of the theoretical investigations is briefly set forth in this article.

Descriptors:

Subject Categories:

• Combustion and Ignition
• Rocket Propellants
• Liquid Rocket Propellants

Distribution Statement:

[A, Approved For Public Release]