MIL-STD-8591 Base Document:2005
Current
The latest, up-to-date edition.
Airborne Stores, Suspension Equipment and Aircraft-Store Interface (Carriage Phase)
12-12-2005
FOREWORD
1. SCOPE
2. APPLICABLE DOCUMENTS
3. DEFINITIONS AND SYMBOLS
4. GENERAL REQUIREMENTS
5. DETAILED REQUIREMENTS
6. NOTES
APPENDIX
A. CARRIAGE DESIGN LIMIT LOADS, GENERAL CASE
B. CARRIAGE DESIGN LIMIT LOADS, STORES CARRIED
ON SPECIFIC AIRCRAFT, A GROUP OR CLASS OF
AIRCRAFT
C. CARRIAGE DESIGN LIMIT LOADS - STORES CARRIED
ON HELICOPTERS
CONCLUDING MATERIAL
Describes general structural and mechanical design criteria for airborne stores, suspension equipment and their associated interfaces.
| DevelopmentNote |
Supersedes MIL A 8591 (H). (12/2005) NOTICE 1 - Notice of Validation. (09/2010) NOTICE 2 - Notice of Validation. (08/2017) New child NOT 3 2022 is added
|
| DocumentType |
Standard
|
| Pages |
73
|
| ProductNote |
New child NOT 3 2022 is added
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
This standard sets forth general structural and mechanical design criteria for airborne stores, suspension equipment and their associated interfaces. Provisions are included to promote interoperability among military aircraft of all Services of the Department of Defense and NATO members\' aircraft. Requirements are provided for design, analysis, and testing of airborne stores, suspension equipment and the aircraft-store interface during captive operations.
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