- Standards Public Review
- 1. Requirements for Aircraft On Board Weight and Balance System
- 2. Guidelines for Mass Properties Control on International Space & Missile Systems
- 5. Mass Properties Control System for Wheeled and Tracked Vehicles
- 6. Standard Coordinate Systems for Reporting the Mass Properties of Flight Vehicles
- 7. Mass Properties Management and Control for Military Aircraft
- 8. Weight and Balance Data Reporting Forms for Aircraft (including Rotorcraft)
- 9. Weight and Balance Control for Guided Missiles
- 10. Weight and Balance Data Reporting Forms for Guided Missiles and Space Launch Vehicles
- 11. Mass Properties Control for Space Vehicles
- 12. Weight Control Technical Requirements for Surface Ships
- 13. Standard Coordinate System for Reporting Mass Properties of Marine Vehicles
- 14. Weight Estimating and Margin Manual for Marine Vehicles
- 15. Vendor Weight Control for the Marine Industry
- 16. Measurement of Missile and Spacecraft Mass Properties
- 17. Weight Distribution and Moments of Inertia for Marine Vehicles
- 100. Vendor Weight Control for the Aircraft Industry
- M-9. Shipboard Weight Surveys
- TO-1. Overview of Mass Properties Engineering for Vehicle Systems
13. Standard Coordinate System for Reporting Mass Properties of Marine Vehicles
Date Issued:
8 November 2009
Revision:
1.1
Prepared by:
Government/Industry Workshop
Society of Allied Weight Engineers, Inc.
Description:
The scope of this Recommended Practice is to establish acceptable three-coordinate reference systems for marine vehicles. Each coordinate system will include a defined origin, specified axes of rotation, and a sign convention in order to establish uniformity in mass property data collection and reporting. The use of a standard coordinate system will minimize the possibility of error due to differences in coordinate systems used by suppliers, designers, builders, regulatory bodies, or owners. These coordinate systems will be used in the determination of centers-of-gravity. They will also be used to determine weight moments of inertia as they relate to the three rotational degrees of freedom: roll, pitch and yaw.
| Attachment | Size |
|---|---|
| SAWE Recommended Practice 13 - 8 Nov 2009 (pdf) | 455.2 KB |











