DI-SESS-81235B

Calculated Weight and Balance Report - Mass Properties Data for Missiles

Specifies requirements for a Calculated Weight and Balance Report providing mass properties data for missiles to control and manage mass characteristics and minimize mass properties variations.

Approval DateAugust 28, 2019

AMSC NumberN10079

Preparing ActivityAS

Project NumberSESS-2019-041

OPR—

DTIC Applicable—

GIDEP Applicable—

Limitation—

Applicable Forms—

Approval Limitation—

Form Version—

DID Formatfree_text

963C CompliantYes

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited.

Supersedes

DI-GDRQ-81235A

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Description & Purpose

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Application & Interrelationship

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Use & Relationship

Weight and Balance Reports are required to provide for control and management of mass characteristics and to ensure minimal mass properties variations

This Data Item Description (DID) contains the format, content, and intended use information for the data deliverable resulting from the work task described in the contract.

This DID supersedes DI-GDRQ-81235A.

Copies of S.A.W.E documents can be obtained from the Society of Allied Weight Engineers, Inc., 375 Redondo Ave., Unit #624, Long Beach, CA, 90814.

Preparation Instructions

1Reference DocumentsThe applicable issue of the documents cited herein, including their approval dates and dates of any applicable amendments, notices, and revisions, shall be as specified in the contract.

2FormatThe report shall be in contractor's format.

3ContentThe Calculated Weight and Balance Report shall be in accordance with the requirements of Society of Allied Weight Engineers (SAWE) Recommended Practice (R.P.) No. 9.

3.1The weight statements in SAWER.P. No. 10, Parts I and II, shall be used for the Calculated Report.

3.2This report shall contain the maximumand minimum weights and moments, with tolerances, for each section, that must be held in order to achieve the desired weight and center of gravity of the assembled missile.

3.3The report shall also contain datato show the weight and balance impact of the complete missile installation on the specified launching aircraft. These data shall be in detail such that the Government can identify the individual electronic units, launching equipment, etc., as well derive the gross weights for the missile carrying conditions (s).

References

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