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The plume impingement test program at AEDC utilizing the S-2 ullage motors (November 1973), section 1Proposed experiments for analyzing rocket plumes are reported. Two groups of experiments were studied: (1) those that would help define some of the parameters that characterize the plume and (2) those that would enable evaluation of some of the contamination effects of the plume environment on various items of interest. The items investigated, the purpose of the investigation, are given in tabular form.
Document ID
19760009082
Acquisition Source
Legacy CDMS
Document Type
Other
Date Acquired
August 8, 2013
Publication Date
January 12, 1976
Publication Information
Publication: The Effects of Solid Rocket Motor Effluents on Selected Surfaces and Solid Particle Size, Distribution, and Composition for Simulated Shuttle Booster Separation Motors
Subject Category
Spacecraft Propulsion And Power
Accession Number
76N16170
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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