- Papers
- Recommended Practices
- 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
- Recommended Practices Public Review
- 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
- Publications
10. Weight and Balance Data Reporting Forms for Guided Missiles and Space Launch Vehicles
Date Issued:
2 May 1997
Revision:
1
Prepared by:
Government/Industry Workshop
Society of Allied Weight Engineers
Description:
This document establishes weight statements and forms for procurement of weight and balance data for guided missiles, PARTS I, II and III hereof, states the principles followed in the formulation of these statements and forms, furnishes instructions where necessary for uniform compilation of the required weight and descriptive data, and provides a glossary of terms for which definitions may not be self evident on the weight statements and forms. The forms may be used for large and small missiles as well as booster vehicles employed for launching satellite or reentry payloads.
Notes:
NOTE: This draft, dated 02 MAY 97, prepared by The Society of Allied Weight Engineers has not been approved and is subject to modification.
| Attachment | Size |
|---|---|
| SAWE_RP10_PART2_02May1997.pdf | 358.88 KB |
| SAWE_RP10_PART1_02May1997.pdf | 405.29 KB |





