درباره ما
MIL-DTL-32028
CORD, DETONATING ASSEMBLY
Organization:
NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD)
Year: 1998
Abstract: This specification covers the requirements for the manufacture and acceptance of the Detonating Cord Assemblies. Referred to in this document as DCA. Intended Use: These DCA are components of the Emergency Egress Hatch Removal Systems installed in the MV-22, CV-22 and HV-22 Aircraft. They are the ballistic signal transmission components of the system. The system is designed to provide emergency egress in a post crash environment on land or water. The Primer-High DCA is used to accept mechanical energy from the initiators and convert it to explosive energy. The High-Low DCA acts as a one-way valve in the seat drop function. The High-Gas DCA provides the gas pressure to function the seat drop thruster. No changes to the configuration shall be permitted without the authorization from the Naval Air Systems Command Headquarters AIR-4.6.1, AIR-4.1.1.2 (V-22) and the Bell-Boeing Joint Program Office. Since the Emergency Egress Hatch Removal Systems are designed for use only in military aircraft, there are no commercial applications for the DCA.
Subject: Aluminum
Collections
:
Show full item record
| contributor author | NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD) | |
| date accessioned | 2017-09-04T15:20:33Z | |
| date available | 2017-09-04T15:20:33Z | |
| date copyright | 36102 | |
| date issued | 1998 | |
| identifier other | MWSIIAAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/20486 | |
| description abstract | This specification covers the requirements for the manufacture and acceptance of the Detonating Cord Assemblies. Referred to in this document as DCA. Intended Use: These DCA are components of the Emergency Egress Hatch Removal Systems installed in the MV-22, CV-22 and HV-22 Aircraft. They are the ballistic signal transmission components of the system. The system is designed to provide emergency egress in a post crash environment on land or water. The Primer-High DCA is used to accept mechanical energy from the initiators and convert it to explosive energy. The High-Low DCA acts as a one-way valve in the seat drop function. The High-Gas DCA provides the gas pressure to function the seat drop thruster. No changes to the configuration shall be permitted without the authorization from the Naval Air Systems Command Headquarters AIR-4.6.1, AIR-4.1.1.2 (V-22) and the Bell-Boeing Joint Program Office. Since the Emergency Egress Hatch Removal Systems are designed for use only in military aircraft, there are no commercial applications for the DCA. | |
| language | English | |
| title | MIL-DTL-32028 | num |
| title | CORD, DETONATING ASSEMBLY | en |
| type | standard | |
| page | 21 | |
| status | Active | |
| tree | NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD):;1998 | |
| contenttype | fulltext | |
| subject keywords | Aluminum | |
| subject keywords | Booster Cups | |
| subject keywords | Detonating | |
| subject keywords | Cord Assembly | |
| subject keywords | Flexible Detonating Cord | |
| subject keywords | Gas Generator | |
| subject keywords | Halar | |
| subject keywords | HMX - Homocyclonite | |
| subject keywords | HNS - Hexanitrostilbene | |
| subject keywords | Percussion primer M42C1-979 | |
| subject keywords | Thin Layer Explosive (TLX)® Trademark of OEA Aerospace |