24 May 1996
28 November 1995
CATAPULT, AIRCRAFT EJECTION SEAT, CKU-7/A ASSEMBLY
This specification is approved for use by the Naval Sea Systems Command, Department of the Navy, and is
available for use by all Departments and Agencies of the Department of Defense.
1.1 Scope. This specification covers the requirements for the CKU-7/A Rocket Catapult.
2. APPLICABLE DOCUMENTS
2.1 General. The documents listed in this section are specified in sections 3 and 4 of this specification. This
section does not include documents cited in other sections of this specification or recommended for additional
information or as examples. While every effort has been made to ensure the completeness of this list,
document users are cautioned that they must meet all specified requirements documents specified in sections
3 and 4 of this specification, whether or not they are listed.
2.2 Government documents.
2.2.1 Specifications, standards, and handbooks. The following specifications, standards, and handbooks
form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these
documents are those listed in the issue of the Department of Defense Index of Specifications and Standards
(DODISS) and supplements thereto, cited in the solicitation (see 6.2).
Seat System, Upward Ejection, Aircraft, General Specification for
Pellet, Boron Potassium Nitrate
Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in
improving this document should be addressed to: Commander, Indian Head Division, Naval Surface Warfare Center,
Standardization Branch (Code 8420), 101 Strauss Avenue, Indian Head, MD 20640-5035, by using the
Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by
sending a letter.
DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited.
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