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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
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.
Distribution Statement:
[A, Approved For Public Release]