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Studies of exhaust products from solid propellant rocket motors fired in an environmental chamberExperiments are described in which it was attempted to define the state of HCl when rocket motors using ammonium perchlorate and powdered aluminum filler in the fuel system are fired under various relative humidity conditions. A small, variable load rocket motor was developed so that controlled quantities of exhaust products could be produced in an environmental chamber. A technique is described for distinguishing the difference between HCl existing as a gas or existing as an acid aerosol.
Document ID
19750051283
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Dawbarn, R.
Kinslow, M.
Nutt, K. W.
Pender, C. W.
(ARO, Inc. von Karman Gas Dynamics Facility, Arnold Air Force Station, Tenn., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1974
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: Conference on Aerospace and Aeronautical Meteorology
Location: El Paso, TX
Start Date: November 12, 1974
End Date: November 15, 1974
Accession Number
75A35355
Distribution Limits
Public
Copyright
Other

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