NATO STANAG 4368
IGNITION SYSTEMS FOR ROCKET AND GUIDED MISSILE MOTORS. SAFETY DESIGN REQUIREMENTS - ED 3
| contributor author | NATO - North Atlantic Treaty Organization | |
| date accessioned | 2017-09-04T15:30:44Z | |
| date available | 2017-09-04T15:30:44Z | |
| date copyright | 08/01/2011 | |
| date issued | 2011 | |
| identifier other | AWSWTEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/32168 | |
| description abstract | AIM The aim of this agreement is to standardize the safety design requirements for ignition systems for rocket and guided missile solid propellant motors used in non-nuclear systems. These safety requirements may be applied to ignition systems of other types of motors, as deemed applicable by the National Safety Approving Authorities (NSAA). | |
| language | English | |
| title | NATO STANAG 4368 | num |
| title | IGNITION SYSTEMS FOR ROCKET AND GUIDED MISSILE MOTORS. SAFETY DESIGN REQUIREMENTS - ED 3 | en |
| type | standard | |
| page | 34 | |
| status | Active | |
| tree | NATO - North Atlantic Treaty Organization:;2011 | |
| contenttype | fulltext |

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