DEFSTAN 13-37(PT1)/2(1981) : 1981 AMD 1 1982
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
DESIGN SAFETY PRINCIPLES AND GENERAL DESIGN CRITERIA FOR AIRBORNE WEAPON FUZING SYSTEMS
21-01-1982
12-01-2013
SECTION A - RELATED DOCUMENTS
SECTION B - INTRODUCTION - Design Safety Principles
SECTION C - DEFINITIONS
SECTION D - GENERAL DESIGN CRITERIA
ANNEX A - ASSOCIATED NATIONAL SPECIFICATIONS
ANNEX B - SUBSTANCE OF AGREEMENT
Covers design safety principles and general criteria for fuzing systems, including arming and safety devices used in airborne weapon systems, especially aircraft gun ammunition, unguided aircraft rockets and free fall stores/weapons including bomblet dispensers used by Ministry of Defence.
| DevelopmentNote |
Supersedes DEFSTAN 13-37(PT1)/1(1971) (08/2003)
|
| DocumentType |
Miscellaneous Product
|
| PublisherName |
UK Ministry of Defence Standards
|
| Status |
Withdrawn
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| DEFSTAN 13-37(PT4)/1(1989) : 1989 | DESIGN SAFETY PRINCIPLES - PART 4: GENERAL DESIGN CRITERIA FOR AIRBORNE DISPENSER WEAPONS |
| DEFSTAN 00-970(PT0)/6(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT13)/7(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| DEFSTAN 10-21/1(1976) : 1976 AMD 2 | AIRCRAFT EJECTOR RELEASE UNITS FOR CONVENTIONAL MUNITIONS |
| DEFSTAN 00-970(PT13)/6(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| DEFSTAN 00-970(PT1)SEC9/4(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT A/C - SECTION 9: MILITARY SPECIFIC SYSTEMS |
| DEFSTAN 00-970(PT1)SEC9/6(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 9: MILITARY SPECIFIC SYSTEMS |
| DEFSTAN 00-970(PT13)/3(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| DEFSTAN 10-20/1(1976) : 1976 | SUSPENSION UNITS WITH RELEASE CAPABILITY FOR CONVENTIONAL MUNITIONS CARRIED ON HELICOPTERS |
| DEFSTAN 00-970(PT13)/11(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| DEFSTAN 00-970(PT13)/4(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| DEFSTAN 00-970(PT13)/10(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| DEFSTAN 00-970(PT1)SEC9/5(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 9: MILITARY SPECIFIC SYSTEMS |
| DEFSTAN 00-970(PT13)/12(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| DEFSTAN 00-970(PT13)/8(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| DEFSTAN 00-970(PT13)/5(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| DEFSTAN 00-970(PT13)/9(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| DEFSTAN 00-970(PT0)/5(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 13-37(PT2)/1(1971) : 1971 | DESIGN SAFETY PRINCIPLES FOR FUSING SYSTEMS FOR ALL LAND SERVICE NON-NUCLEAR WEAPONS - PART 2 |
| DEFSTAN 13-91/2(1981) : 1981 AMD 2 | MECHANICAL ARMING WIRE CONNECTIONS BETWEEN AIRBORNE ARMAMENT STORES AND ASSOCIATED SUSPENSION EQUIPMENT |
| DEFSTAN 13-37(PT3)/1(1971) : 1971 | DESIGN SAFETY PRINCIPLES FOR DEMOLITION AND ENGINEERING EXPLOSIVES STORES - PART 3 |
| DEFSTAN 00-970(PT7)SEC3/5(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 3: MILITARY SPECIFIC ITEMS |
| DEFSTAN 00-970(PT7)SEC3/6(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 3: MILITARY SPECIFIC ITEMS |
| DEFSTAN 13-37(PT3)/1(1971) : 1971 | DESIGN SAFETY PRINCIPLES FOR DEMOLITION AND ENGINEERING EXPLOSIVES STORES - PART 3 |
| STANAG 3525 : 0 | SAFETY DESIGN REQUIREMENTS - AIRBORNE FUZING SYSTEMS |
| MIL-STD-1316 Revision F:2017 | Fuze Design, Safety Criteria for |
| DEFSTAN 13-37(PT2)/1(1971) : 1971 | DESIGN SAFETY PRINCIPLES FOR FUSING SYSTEMS FOR ALL LAND SERVICE NON-NUCLEAR WEAPONS - PART 2 |
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