Design and test of a rocket motor expansion joint
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Authors
Reiserer, Russell Lawrence
Barden, Kenneth Perrin
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Date of Issue
1947
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California Institute of Technology
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Abstract
If the science of guided missiles is to continue to
advance, each component part of the missile mast be perfected.
This means that a satisfactory propulsive system capable of
continual operation to some degree must be developed. The
development of a satisfactory expansion joint for the rocket
motor is one phase of this problem.
Type
Thesis
Description
This thesis document was issued under the authority of another institution, not NPS. At the time it was written, a copy was added to the NPS Library collection for reasons not now known. It has been included in the digital archive for its historical value to NPS. Not believed to be a CIVINS (Civilian Institutions) title.
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Rights
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.