Patent ID: 11939151
Assignee: THE UNITED STATES OF AMERICA, AS REPRESENTED BY THE SECRETARY OF THE NAVY
Field: Other special machines (Mechanical engineering)
Classification: CPC B  F | IPC B

Claim 19:
20. The dunnage assembly according to claim 19, further comprising a plurality of cylindrical members, wherein said each of the plurality of cylindrical members is positioned within a corresponding thru-hole in the fuze support collar and is substantially coaxially aligned with a corresponding tube of the forwardmost dunnage section, and
wherein the cylindrical members are accessible at the exterior side of the rocket fuze support collar; and
a pad member being attached to the exterior side of the rocket fuze support collar for covering the cylindrical members and to protect the fuze portion of the rocket,
wherein the fuze support collar includes a plurality of thru-holes therein,
wherein said each of the plurality of thru-holes in the fuze support collar is substantially coaxially aligned with a corresponding thru-hole in the second tube collar, and
wherein said each tube in the forwardmost dunnage section includes a first inner diameter and does not extend into the thru-holes of the fuze support collar, and
wherein said each of the plurality of cylindrical members includes a second inner diameter that is less than the first inner diameter and is sized to receive the fuze portion of a rocket.