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MIL-STD-2131A
LAUNCHER, EJECTION, GUIDED MISSILE AIRCRAFT, GENERAL DESIGN CRITERIA FOR
Organization:
NAVY - AS - Naval Air Systems Command
Year: 1991
Abstract: The purpose of this document is to provide guidelines for establishing general criteria for the design, development, construction, maintenance and testing of an ejection launcher. This standard is applicable to all missile suspension systems. However, it is assumed that all new missile developments will employ a 14-inch or 30-inch missile suspension system as defined in MIL-A-8591. The launcher shall provide for the carriage, service and power ejection release of an airborne guided missile with either a nuclear or conventional warhead from tactical aircraft in flight. Intended Use: The intended use of this standard is to provide guidelines for establishing criteria for the design, development, construction, maintenance, and testing of an ejection launcher.
Subject: Captive flight loads
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| contributor author | NAVY - AS - Naval Air Systems Command | |
| date accessioned | 2017-09-04T15:49:16Z | |
| date available | 2017-09-04T15:49:16Z | |
| date copyright | 33588 | |
| date issued | 1991 | |
| identifier other | QDKWDAAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/52202 | |
| description abstract | The purpose of this document is to provide guidelines for establishing general criteria for the design, development, construction, maintenance and testing of an ejection launcher. This standard is applicable to all missile suspension systems. However, it is assumed that all new missile developments will employ a 14-inch or 30-inch missile suspension system as defined in MIL-A-8591. The launcher shall provide for the carriage, service and power ejection release of an airborne guided missile with either a nuclear or conventional warhead from tactical aircraft in flight. Intended Use: The intended use of this standard is to provide guidelines for establishing criteria for the design, development, construction, maintenance, and testing of an ejection launcher. | |
| language | English | |
| title | MIL-STD-2131A | num |
| title | LAUNCHER, EJECTION, GUIDED MISSILE AIRCRAFT, GENERAL DESIGN CRITERIA FOR | en |
| type | standard | |
| page | 40 | |
| status | Active | |
| tree | NAVY - AS - Naval Air Systems Command:;1991 | |
| contenttype | fulltext | |
| subject keywords | Captive flight loads | |
| subject keywords | Clearances | |
| subject keywords | Interfaces |