Design and test of a rocket motor expansion joint
Reiserer, Russell Lawrence
Barden, Kenneth Perrin
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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.
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.