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Flow processes in overexpanded chemical rocket nozzles. Part 2: Side loads due to asymmetric separationMethods for measuring the lateral forces, occurring as a result of asymmetric nozzle flow separation, are discussed. The effect of some parameters on the side load is explained. A new method was developed for calculation of the side load. The values calculated are compared with side load data of the J-2 engine. Results are used for predicting side loads of the space shuttle main engine.
Document ID
19840011403
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Schmucker, R. H.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1984
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-TM-77395
TUM-LRT-TB-10
NAS 1.15:77395
Accession Number
84N19471
Funding Number(s)
CONTRACT_GRANT: NASW-3542
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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